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: 1 day ago

TLE from 1 day ago
0 DELTA 1 DEB
1  5975U 70021C   25311.25888874  .00002258  00000-0  12178-2 0  9996
2  5975  25.7207   1.1001 6510043 156.5426 256.5300  3.26265833365667
Epoch: 2025-11-07T06:12Z
TLE epoch observation values (Epoch: 2025-11-07T06:12:47.987Z)
Latitude
0.00004°
Longitude
-138.80422°
Altitude
21,096.61 km
Speed
2.874 km/s
True Right ascension
00h 04m 24s
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
03:48:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
25,331.238 km
Perigee altitude
324.714 km
Semi-major axis
19,206.113 km
Eccentricity
0.651
Inclination
25.7207°
RAAN
1.1001°
Arg. of periapsis
156.5426°
True anomaly
203.43697°
Mean anomaly
256.53°
Eccentric anomaly
228.56576°
Mean motion
0.81542 °/min
Orbital period
441.49 mins
BSTAR
0.0012178
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Other satellites on launch #21 in the year 1970 (1970-03-20 UTC)

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