DELTA 1 R/B, 50

Orbit data source: Space-Track

DELTA 1 R/B, 50 is space debris in LEO originally from a launch on Fri, 12 Aug 1960 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
50, 1960-009B
Orbit
LEO
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)
1960-08-12 (65 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 DELTA 1 R/B
1    50U 60009B   25318.70500350 -.00000053  00000-0  31349-3 0  9991
2    50  47.2286 107.4640 0113871  95.8415 265.5368 12.20161787911518
Epoch: 2025-11-14T16:55Z
TLE epoch observation values (Epoch: 2025-11-14T16:55:12.302Z)
Latitude
Longitude
159.61808°
Altitude
1,600.138 km
Speed
7.067 km/s
True Right ascension
07h 09m 51s
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
22:55:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,683.668 km
Perigee altitude
1,502.134 km
Semi-major axis
7,971.038 km
Eccentricity
0.01139
Inclination
47.2286°
RAAN
107.464°
Arg. of periapsis
95.8415°
True anomaly
264.23744°
Mean anomaly
265.5368°
Eccentric anomaly
264.88696°
Mean motion
3.0498 °/min
Orbital period
118.04 mins
BSTAR
0.00031349
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