DELTA 1 R/B, 6921

Orbit data source: Space-Track

DELTA 1 R/B, 6921 is space debris in SSO originally from a launch on Tue, 06 Nov 1973 UTC launched from the Air Force Western Test Range (AFWTR). 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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Identifier
6921, 1973-086B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Aerojet
Mission
Spacecraft
Bus & Motor
DSV-3E-5, AJ10-118F
Mass
756 kg wet, 756 kg dry
Launch date (UTC)
1973-11-06 (52 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 DELTA 1 R/B
1 06921U 73086B   26084.56672245 -.00000042  00000-0  29388-4 0  9990
2 06921 102.3487 113.9026 0014852  63.3793 296.8788 12.37066488379998
Epoch: 2026-03-25T13:36Z
TLE epoch observation values (Epoch: 2026-03-25T13:36:04.819Z)
Latitude
0.00005°
Longitude
86.85433°
Altitude
1,516.305 km
Speed
7.109 km/s
True Right ascension
07h 35m 36s
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
02:38:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,528.388 km
Perigee altitude
1,504.937 km
Semi-major axis
7,894.8 km
Eccentricity
0.00149
Inclination
102.3487°
RAAN
113.9026°
Arg. of periapsis
63.3793°
True anomaly
296.72687°
Mean anomaly
296.8788°
Eccentric anomaly
296.80285°
Mean motion
3.09408 °/min
Orbital period
116.35 mins
BSTAR
0.000029388
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