DELTA 1 R/B(1), 10144

Orbit data source: Space-Track

DELTA 1 R/B(1), 10144 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
10144, 1977-065B
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)
1977-07-14 (49 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL + SKIRT + NOZZLE, 1.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 DELTA 1 R/B(1)
1 10144U 77065B   26263.06881395  .00000929  00000-0  24886-3 0  9995
2 10144  29.0642 252.9414 0839514 307.7772  44.9586 13.26101346375508
Epoch: 2026-09-20T01:39Z
TLE epoch observation values (Epoch: 2026-09-20T01:39:05.525Z)
Latitude
-0°
Longitude
-130.79992°
Altitude
741.195 km
Speed
7.691 km/s
True Right ascension
16h 51m 45s
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
04:41:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,798.609 km
Perigee altitude
532.04 km
Semi-major axis
7,543.461 km
Eccentricity
0.08395
Inclination
29.0642°
RAAN
252.9414°
Arg. of periapsis
307.7772°
True anomaly
52.27932°
Mean anomaly
44.9586°
Eccentric anomaly
48.56472°
Mean motion
3.31274 °/min
Orbital period
108.67 mins
BSTAR
0.00024886
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