**DELTA 1 R/B(2) *, 11792**

Orbit data source: Space-Track

DELTA 1 R/B(2) *, 11792 is space debris in HEO originally from a launch on Wed, 26 Oct 1966 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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<iframe src="https://www.satcat.com/sats-embedded/11792?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/11792?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

11792, 1966-096C

Orbit

HEO

Country

Related business

European Space Agency (FR)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-10-26 (60 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 1.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 5 days ago

TLE from 5 days ago

0 DELTA 1 R/B(2) *
1 11792U 66096C   26249.41834532  .00000806  00000-0  10631-2 0  9997
2 11792  17.8048 358.8809 6052548  25.3055 354.8448  3.84771769434516

Epoch: 2026-09-06T10:02Z

TLE epoch observation values (Epoch: 2026-09-06T10:02:25.035Z)

Latitude

-0.00007°

Longitude

-137.23496°

Altitude

665.034 km

Speed

9.487 km/s

True Right ascension

23h 55m 31s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

07:29:19

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

21,243.799 km

Perigee altitude

414.322 km

Semi-major axis

17,207.197 km

Eccentricity

0.60525

Inclination

17.8048°

RAAN

358.8809°

Arg. of periapsis

25.3055°

True anomaly

334.32807°

Mean anomaly

354.8448°

Eccentric anomaly

347.10686°

Mean motion

0.96156 °/min

Orbital period

374.39 mins

BSTAR

0.0010631

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Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)

INTELSAT 2-F1, 2514

DELTA 1 R/B(1), 2515 (Decayed)

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DELTA 1 R/B(2) * Visibility forecast

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Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
158 mins	2026-09-11 15:07:12.012Z	228.826° WSW	2026-09-11 15:20:12.012Z	166.587° S	37.231°	2026-09-11 17:45:12.012Z	124.288° SE
187 mins	2026-09-11 22:23:12.012Z	247.022° WSW	2026-09-11 23:21:12.012Z	234.189° WSW	14.942°	2026-09-12 01:30:12.012Z	220.37° SW

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out DELTA 1 R/B(2) *, 11792 on other resources

View DELTA 1 R/B(2) *, 11792 on Heavens-Above

View DELTA 1 R/B(2) *, 11792 on Keep Track

View DELTA 1 R/B(2) *, 11792 on Celestrak

View DELTA 1 R/B(2) *, 11792 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

DELTA 1 R/B(2) *, 11792

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 5 days ago

TLE from 5 days ago

TLE epoch observation values (Epoch: 2026-09-06T10:02:25.035Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)

DELTA 1 R/B(2) * Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 R/B(2) *, 11792 on other resources

Documentation

**DELTA 1 R/B(2) *, 11792**

Expand to show TLE details & history
Last TLE update: 5 days ago