**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 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 DELTA 1 R/B(2) *
1 11792U 66096C   26073.58079305  .00004942  00000-0  56124-2 0  9991
2 11792  17.6808 127.6060 6059609 146.4216 273.5375  3.84300881427744

Epoch: 2026-03-14T13:56Z

TLE epoch observation values (Epoch: 2026-03-14T13:56:20.519Z)

Latitude

-0°

Longitude

106.33318°

Altitude

15,622.455 km

Speed

3.617 km/s

True Right ascension

08h 30m 28s

True Declination

0° 00' 00"

Sunlit

Object was in daylight 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

18:44:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

21,278.536 km

Perigee altitude

407.714 km

Semi-major axis

17,221.262 km

Eccentricity

0.60596

Inclination

17.6808°

RAAN

127.606°

Arg. of periapsis

146.4216°

True anomaly

213.57672°

Mean anomaly

273.5375°

Eccentric anomaly

242.68873°

Mean motion

0.96039 °/min

Orbital period

374.85 mins

BSTAR

0.0056124

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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.
283 mins	2026-03-15 23:43:05.567Z	199.426° SSW	2026-03-16 03:35:05.567Z	162.142° S	30.845°	2026-03-16 04:26:05.567Z	110.621° ESE
12 mins	2026-03-16 10:48:05.567Z	243.817° WSW	2026-03-16 10:56:05.567Z	213.469° SW	15.509°	2026-03-16 11:00:05.567Z	179.838° S

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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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-03-14T13:56:20.519Z)

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: 1 day ago