**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 URL

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

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ISO8601 Format

Identifier

11792, 1966-096C

Orbit

HEO

Last TLE update

14 hours ago

Origin

European Space Agency (US)

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

Cyl, 1.5 m

Radar Cross Section

0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 14 hours ago

0 DELTA 1 R/B(2) *
1 11792U 66096C   25181.82065017  .00010143  00000-0  81184-2 0  9996
2 11792  17.9419 316.8127 6123261 156.0280 252.5288  3.77961873417931

Epoch: 2025-06-30T19:41Z

TLE epoch observation values (Epoch: 2025-06-30T19:41:44.174Z)

Latitude

0.00001°

Longitude

102.24651°

Altitude

18,314.486 km

Speed

3.064 km/s

True Right ascension

21h 07m 13s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

17.40167°

Longitude

176.31162°

Altitude

3,596.066 km

Speed

7.552 km/s

Apparent Right ascension

04h 06m 01s

Apparent Declination

-7° 03' 57"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:33:54

Azimuth

90.317° ESE

Elevation

-10.674°

Doppler factor

Orbital elements

Apogee altitude

21,697.689 km

Perigee altitude

372.523 km

Semi-major axis

17,413.243 km

Eccentricity

0.61233

Inclination

17.9419°

RAAN

316.8127°

Arg. of periapsis

156.028°

True anomaly

Unknown

Mean anomaly

252.5288°

Eccentric anomaly

Unknown

Mean motion

0.94455 °/min

Orbital period

381.13 mins

BSTAR

0.0081184

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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)

DELTA 1 R/B(2) * Visibility forecast

Observer location: undefined°, undefined°

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.
26 mins	2025-07-01 16:01:32.867Z	253.98° W	2025-07-01 16:21:32.867Z	216.383° SW	21.213°	2025-07-01 16:27:32.867Z	171.412° S
206 mins	2025-07-02 06:29:32.867Z	205.331° SW	2025-07-02 09:55:32.867Z	186.238° SSW	32.574°	2025-07-02 09:55:32.867Z	186.238° SSW

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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.