---
analysis-role: source-anchored-analysis
analysis-category: document-telemetry
confidence-level: medium
ai-analysis: true
accuracy-disclaimer: AI-assisted analysis; interpretations are provisional and may contain errors. Verify against cited source material.
ai-generated: true
companion-eligible: true
topic-slug: d74-syria-november-2023-page-10-telemetry-anchor
topic-title: D74 Syria November 2023 Page 10 Telemetry Anchor
topic-description: Page-level review of the Syria November 2023 mission report telemetry row: 424-knot estimated velocity, near co-altitude pass, seven-minute observation, and no emissions.
guide-description: Uses the captured page as a control row for modern military telemetry and field-obscuration synthesis without upgrading it to physical propulsion proof.
topic-audience: serious-uap-readers
topic-priority: 8
---

# D74 Syria November 2023 Page 10 Telemetry Anchor

![D74 Syria November 2023 page 10 source rendering](/media/Release_1/Analysis/images/dow-uap-d74-page10-mission-report-source-page.png)

## Source Basis

The source is [Mission Report, Syria, November 2023](/?open=Release_1%2FDOW-UAP-D74-Mission-Report-Syria-November-2023.pdf&page=10), page 10 of 10. The approved capture lead requested a page-only document review with readability adjustment, using [the captured viewer state](/?open=Release_1%2FDOW-UAP-D74-Mission-Report-Syria-November-2023.pdf&page=10&docZoom=0.5670961464860429&rotation=0).

This note links the page-level finding back to the existing synthesis targets: [18 - Theoretical Craft Prototypes / Field-Obscuration Synthesis](/?open=Release_2%2FAnalysis%2F18-Theoretical-Craft-Prototypes-Field-Obscuration-Synthesis.md), [C00 - Executive Disclosure Synthesis](/?open=Release_2%2FAnalysis%2FC00-Executive-Disclosure-Synthesis.md), [C03 - Modern Military Operational Cases](/?open=Release_2%2FAnalysis%2FC03-Modern-Military-Operational-Cases.md), [C07 - Field Propulsion and Morphology Model](/?open=Release_2%2FAnalysis%2FC07-Field-Propulsion-and-Morphology-Model.md), [C24 - Physics Exploration Summary](/?open=Release_2%2FAnalysis%2FC24-Physics-Exploration-Summary.md), and [C43 - Flight Characteristics and Telemetry Observations Summary](/?open=Release_2%2FAnalysis%2FC43-Flight-Characteristics-and-Telemetry-Observations-Summary.md).

## Observation

Page 10 records a recommendation by USCENTCOM Chief of Staff MG Brandon R. Tegtmeier, recommended on 2 June 2025, with operational details for a November 2023 Syria probable-UAP event. The visible page fields support the following source-observable row:

| Field | Page-10 read | Analysis boundary |
| --- | --- | --- |
| Acquisition time | `092153:00ZNOV23` | Treat as the source record's event timestamp, not an independent sensor replay. |
| Velocity | `424KN`, with velocity accuracy marked estimated | Strong enough for telemetry comparison; not enough for acceleration or propulsion calculation. |
| Relative geometry | The event text says the probable UAP came from the south at near co-altitude, dropped altitude, and safely passed the aircraft. | Supports altitude-behavior language but lacks range, platform track, sensor pointing, and exact closest approach. |
| Duration | The aircrew watched for about seven minutes before the probable UAP became out of range. | Important because the row is sustained, not a one-frame visual impression. |
| Emissions/effects | The page says no emissions came from the probable UAP, it was not considered a threat to aircraft or public safety, and it had no effects on the aircrew. | Supports a no-emissions operational-control lane; it does not prove exotic propulsion. |
| Description | The source text describes one probable high-confidence UAP shaped as a "bouncy ball"; redactions obscure some fields. | Shape language is useful but not enough for hull morphology without imagery. |

## Hypothesis To Test

The approved lead asks what page 10 supports or weakens. It supports a stronger document-telemetry anchor for the Syria November 2023 row already cited by [C43 - Flight Characteristics and Telemetry Observations Summary](/?open=Release_2%2FAnalysis%2FC43-Flight-Characteristics-and-Telemetry-Observations-Summary.md): a sustained, estimated 424-knot near-co-altitude pass, with reported altitude drop, safe aircraft pass, seven-minute observation, and no emissions or aircrew effects.

It weakens any attempt to treat the row as measured propulsion proof. The page does not expose sensor mode, range, platform state, trackfile details, native replay frames, or a physical body outline. The strongest promotion is "high-value sustained-flight telemetry row with no-emissions language," not "confirmed field craft."

## Modern Military Tie-In

[C03 - Modern Military Operational Cases](/?open=Release_2%2FAnalysis%2FC03-Modern-Military-Operational-Cases.md) should treat D74 as one of the stronger Release 1 operational rows because it combines mission context, speed, duration, relative altitude behavior, and a benign/no-emissions assessment. The case belongs beside Greece January 2024 SWIR-only visibility, Iraq 2023 dimming/disappearance, and Arabian Gulf telemetry rows.

For [C43 - Flight Characteristics and Telemetry Observations Summary](/?open=Release_2%2FAnalysis%2FC43-Flight-Characteristics-and-Telemetry-Observations-Summary.md), this page-level review sharpens the existing Syria row: the useful pattern is not just `424KN`, but `424KN` plus seven minutes, near co-altitude, altitude drop, out-of-range termination, no emissions, and no reported aircrew effect.

## Theoretical Scene Panels

| Panel | Source-grounded read | Speculative model | Limit |
| --- | --- | --- | --- |
| A - Page 10 telemetry row | The page records an estimated 424-knot probable UAP pass in Syria at `092153:00ZNOV23`. | A compact object or observable envelope may have held aircraft-relevant speed while remaining operationally benign. | The page is not a sensor track and does not provide range or attitude. |
| B - Near co-altitude pass | The text says the probable UAP came from the south at near co-altitude, dropped altitude, and safely passed the aircraft. | A controlled flight path is possible; the event should be compared against conventional aircraft, balloon, drone, and sensor/reporting controls. | No map, platform track, or closest-approach geometry is visible on this page. |
| C - No-emissions control | The source says no emissions came from the probable UAP and no effects were reported on the aircrew. | Under a field-obscuration model, absence of conventional emissions is a useful targeting clue. | "No emissions reported" is not the same as "no emissions physically existed." |
| D - Synthesis bridge | The row links modern military telemetry to field/body hypotheses. | It can inform prototype and propulsion models as a document anchor. | It should not outrank frame-derived or instrument-derived evidence. |

## Working Assessment

This page should be promoted as a durable telemetry anchor. It strengthens the modern-military and field-obscuration comparison set because it combines sustained duration, estimated speed, relative altitude behavior, and no-emissions language in one local source page.

The Disclosure-Forward Neutrality Gate passes: ordinary aircraft/drone/reporting controls remain live because the page lacks geometry and sensor replay, while a disclosure-forward low-emission or field-mediated flight model remains a testable comparison lane. The next upgrade would require adjacent pages, trackfile/sensor metadata, or paired video that confirms the relative motion and observation geometry.

## Follow-Up

- Add page anchors for the D74 row wherever [C43 - Flight Characteristics and Telemetry Observations Summary](/?open=Release_2%2FAnalysis%2FC43-Flight-Characteristics-and-Telemetry-Observations-Summary.md) later builds a structured telemetry CSV.
- Compare D74 against [Mission Report, Greece, January 2024](/?open=Release_1%2FDOW-UAP-D25-Mission-Report-Greece-January-2024.pdf) because both rows combine aircraft-relevant speed with a nonstandard observability/control claim.
- Do not use D74 as a standalone propulsion proof unless future source material exposes range, platform state, sensor mode, and track continuity.