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 via an FALCON 9 launch vehicle 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 (49 years ago)
Launch vehicle
FALCON 9
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: 5 hours ago

TLE from 5 hours ago
0 DELTA 1 R/B(1)
1 10062U 77048B   26256.55910327  .00000194  00000-0  38077-4 0  9991
2 10062  28.4183   2.6967 0726388  13.3807 348.4961 13.39083350398878
Epoch: 2026-09-13T13:25Z
TLE epoch observation values (Epoch: 2026-09-13T13:25:06.522Z)
Latitude
Longitude
168.86751°
Altitude
579.774 km
Speed
7.836 km/s
True Right ascension
00h 10m 47s
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
11:19:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,661.025 km
Perigee altitude
572.205 km
Semi-major axis
7,494.752 km
Eccentricity
0.07264
Inclination
28.4183°
RAAN
2.6967°
Arg. of periapsis
13.3807°
True anomaly
346.67494°
Mean anomaly
348.4961°
Eccentric anomaly
347.60258°
Mean motion
3.34509 °/min
Orbital period
107.62 mins
BSTAR
0.000038077
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