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: 13 hours ago

TLE from 13 hours ago
0 DELTA 1 R/B
1 06921U 73086B   26034.50850143 -.00000035  00000-0  90030-4 0  9998
2 06921 102.3558  63.4229 0014951 153.0290 207.1550 12.37065297373803
Epoch: 2026-02-03T12:12Z
TLE epoch observation values (Epoch: 2026-02-03T12:12:14.523Z)
Latitude
-0.00004°
Longitude
106.67397°
Altitude
1,532.11 km
Speed
7.095 km/s
True Right ascension
04h 13m 41s
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
03:14:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,528.472 km
Perigee altitude
1,504.865 km
Semi-major axis
7,894.805 km
Eccentricity
0.0015
Inclination
102.3558°
RAAN
63.4229°
Arg. of periapsis
153.029°
True anomaly
207.07694°
Mean anomaly
207.155°
Eccentric anomaly
207.11596°
Mean motion
3.09408 °/min
Orbital period
116.35 mins
BSTAR
0.00009003
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