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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 DELTA 1 R/B
1 00050U 60009B   26098.09577641 -.00000046  00000-0  37401-3 0  9993
2 00050  47.2339  19.2836 0113015 166.1328 194.2606 12.20163136929140
Epoch: 2026-04-08T02:17Z
TLE epoch observation values (Epoch: 2026-04-08T02:17:55.081Z)
Latitude
-0.00001°
Longitude
148.44103°
Altitude
1,679.397 km
Speed
6.997 km/s
True Right ascension
01h 17m 08s
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
07:39:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,682.979 km
Perigee altitude
1,502.81 km
Semi-major axis
7,971.032 km
Eccentricity
0.0113
Inclination
47.2339°
RAAN
19.2836°
Arg. of periapsis
166.1328°
True anomaly
193.9459°
Mean anomaly
194.2606°
Eccentric anomaly
194.10282°
Mean motion
3.0498 °/min
Orbital period
118.04 mins
BSTAR
0.00037401
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