DELTA 1 R/B(1), 10062

Orbit data source: Space-Track

DELTA 1 R/B(1), 10062 is space debris in LEO originally from a launch on Thu, 16 Jun 1977 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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Identifier
10062, 1977-048B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
MDAC-HB
Mission
Spacecraft
Bus & Motor
DELTA/TR-201, Unknown motor
Mass
845 kg wet, 845 kg dry
Launch date (UTC)
1977-06-16 (48 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
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 DELTA 1 R/B(1)
1 10062U 77048B   25306.25510660  .00000380  00000-0  10036-3 0  9990
2 10062  28.4185 156.5802 0727780 296.0770  56.6649 13.38792244356584
Epoch: 2025-11-02T06:07Z
TLE epoch observation values (Epoch: 2025-11-02T06:07:21.210Z)
Latitude
-0.00003°
Longitude
22.96831°
Altitude
841.988 km
Speed
7.567 km/s
True Right ascension
10h 26m 19s
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
14:13:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,663.232 km
Perigee altitude
572.168 km
Semi-major axis
7,495.837 km
Eccentricity
0.07278
Inclination
28.4185°
RAAN
156.5802°
Arg. of periapsis
296.077°
True anomaly
63.97832°
Mean anomaly
56.6649°
Eccentric anomaly
60.2865°
Mean motion
3.34436 °/min
Orbital period
107.64 mins
BSTAR
0.00010036
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