DELTA 1 DEB, 39100

Orbit data source: Space-Track

DELTA 1 DEB, 39100 is space debris in LEO originally from a launch on Thu, 14 Jul 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
39100, 1977-065GM
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1977-07-14 (48 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

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

TLE from 2 days ago
0 DELTA 1 DEB
1 39100U 77065GM  25304.47890233  .00013286  00000-0  10749-2 0  9991
2 39100  29.2776  35.0144 0349914 321.3542  36.2489 14.61016577698581
Epoch: 2025-10-31T11:29Z
TLE epoch observation values (Epoch: 2025-10-31T11:29:37.161Z)
Latitude
0.00001°
Longitude
-177.41316°
Altitude
492.034 km
Speed
7.726 km/s
True Right ascension
02h 20m 03s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
00:12:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
941.363 km
Perigee altitude
446.442 km
Semi-major axis
7,072.04 km
Eccentricity
0.03499
Inclination
29.2776°
RAAN
35.0144°
Arg. of periapsis
321.3542°
True anomaly
38.70562°
Mean anomaly
36.2489°
Eccentric anomaly
37.46851°
Mean motion
3.64944 °/min
Orbital period
98.65 mins
BSTAR
0.0010749
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