DELTA 1 DEB, 5975

Orbit data source: Space-Track

DELTA 1 DEB, 5975 is space debris in HEO originally from a launch on Fri, 20 Mar 1970 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
5975, 1970-021C
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1970-03-20 (56 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 DELTA 1 DEB
1 05975U 70021C   26138.62049305  .00002412  00000-0  11317-2 0  9999
2 05975  25.5765 250.7691 6511198 343.9125   2.6067  3.26994162371954
Epoch: 2026-05-18T14:53Z
TLE epoch observation values (Epoch: 2026-05-18T14:53:30.599Z)
Latitude
0.00002°
Longitude
151.06378°
Altitude
403.606 km
Speed
9.836 km/s
True Right ascension
16h 42m 59s
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
12:54:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
25,286.397 km
Perigee altitude
312.552 km
Semi-major axis
19,177.611 km
Eccentricity
0.65112
Inclination
25.5765°
RAAN
250.7691°
Arg. of periapsis
343.9125°
True anomaly
16.08585°
Mean anomaly
2.6067°
Eccentric anomaly
7.43274°
Mean motion
0.81724 °/min
Orbital period
440.51 mins
BSTAR
0.0011317
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Other satellites on launch #21 in the year 1970 (1970-03-20 UTC)

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