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 (66 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 DELTA 1 R/B
1 00050U 60009B   26313.73974375 -.00000100  00000-0 -12728-3 0  9996
2 00050  47.2307  69.9290 0113485  89.1416 272.2375 12.20170128955478
Epoch: 2026-11-09T17:45Z
TLE epoch observation values (Epoch: 2026-11-09T17:45:13.859Z)
Latitude
0.00007°
Longitude
114.70935°
Altitude
1,589.509 km
Speed
7.076 km/s
True Right ascension
04h 39m 42s
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
04:31:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,683.324 km
Perigee altitude
1,502.406 km
Semi-major axis
7,971.002 km
Eccentricity
0.01135
Inclination
47.2307°
RAAN
69.929°
Arg. of periapsis
89.1416°
True anomaly
270.93744°
Mean anomaly
272.2375°
Eccentric anomaly
271.58753°
Mean motion
3.04982 °/min
Orbital period
118.04 mins
BSTAR
-0.00012728
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