DELTA 1 R/B, 515

Orbit data source: Space-Track

DELTA 1 R/B, 515 is space debris originally from a launch on Thu, 13 Dec 1962 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
515, 1962-068B
Orbit
Active
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
24 kg wet, 24 kg dry
Launch date (UTC)
1962-12-13 (63 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

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

TLE from 2 days ago
0 DELTA 1 R/B
1 00515U 62068B   25260.23539502 -.00000017  00000-0  00000-0 0  9996
2 00515  47.5291 347.7502 2831624 307.4626  30.0060  7.79266622786572
Epoch: 2025-09-17T05:38Z
TLE epoch observation values (Epoch: 2025-09-17T05:38:58.129Z)
Latitude
-0.00002°
Longitude
-93.40628°
Altitude
2,057.134 km
Speed
7.579 km/s
True Right ascension
23h 11m 00s
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
00:19:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
7,412.814 km
Perigee altitude
1,326.166 km
Semi-major axis
10,747.627 km
Eccentricity
0.28316
Inclination
47.5291°
RAAN
347.7502°
Arg. of periapsis
307.4626°
True anomaly
52.60694°
Mean anomaly
30.006°
Eccentric anomaly
40.55435°
Mean motion
1.94793 °/min
Orbital period
184.81 mins
BSTAR
0
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Other satellites on launch #68 in the year 1962 (1962-12-13 UTC)

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