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: 6 hours ago

TLE from 6 hours ago
0 DELTA 1 R/B
1    50U 60009B   25304.86371649 -.00000047  00000-0  37653-3 0  9997
2    50  47.2278 150.4305 0113917  54.4519 306.6830 12.20161200909824
Epoch: 2025-10-31T20:43Z
TLE epoch observation values (Epoch: 2025-10-31T20:43:45.104Z)
Latitude
-0.00001°
Longitude
159.09052°
Altitude
1,538.49 km
Speed
7.122 km/s
True Right ascension
10h 01m 43s
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
21:58:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,683.708 km
Perigee altitude
1,502.1 km
Semi-major axis
7,971.041 km
Eccentricity
0.01139
Inclination
47.2278°
RAAN
150.4305°
Arg. of periapsis
54.4519°
True anomaly
305.62722°
Mean anomaly
306.683°
Eccentric anomaly
306.156°
Mean motion
3.04979 °/min
Orbital period
118.04 mins
BSTAR
0.00037653
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