DELTA 1 DEB, 10184

Orbit data source: Space-Track

DELTA 1 DEB, 10184 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
10184, 1977-065N
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1977-07-14 (49 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.7 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 DELTA 1 DEB
1 10184U 77065N   26133.18037378  .00001131  00000-0  24971-3 0  9993
2 10184  29.0787  93.4237 0755305 310.5465  43.1660 13.49398475362538
Epoch: 2026-05-13T04:19Z
TLE epoch observation values (Epoch: 2026-05-13T04:19:44.294Z)
Latitude
-0.00003°
Longitude
157.54499°
Altitude
684.082 km
Speed
7.71 km/s
True Right ascension
06h 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
19:12:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,641.518 km
Perigee altitude
515.137 km
Semi-major axis
7,456.464 km
Eccentricity
0.07553
Inclination
29.0787°
RAAN
93.4237°
Arg. of periapsis
310.5465°
True anomaly
49.5105°
Mean anomaly
43.166°
Eccentric anomaly
46.29441°
Mean motion
3.37088 °/min
Orbital period
106.8 mins
BSTAR
0.00024971
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