DELTA 1 DEB *, 5987

Orbit data source: Space-Track

DELTA 1 DEB *, 5987 is space debris in HEO originally from a launch on Wed, 11 Jan 1967 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
5987, 1967-001S
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1967-01-11 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 DELTA 1 DEB *
1 05987U 67001S   25285.15359767  .00000069  00000-0  75578-3 0  9998
2 05987  26.3550 255.8588 6706488 103.6853 334.0510  2.88984615371589
Epoch: 2025-10-12T03:41Z
TLE epoch observation values (Epoch: 2025-10-12T03:41:10.838Z)
Latitude
0.00002°
Longitude
179.50663°
Altitude
7,229.81 km
Speed
6.28 km/s
True Right ascension
17h 03m 06s
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
07:45:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
28,411.263 km
Perigee altitude
480.235 km
Semi-major axis
20,823.886 km
Eccentricity
0.67065
Inclination
26.355°
RAAN
255.8588°
Arg. of periapsis
103.6853°
True anomaly
256.44582°
Mean anomaly
334.051°
Eccentric anomaly
301.17446°
Mean motion
0.72227 °/min
Orbital period
498.43 mins
BSTAR
0.00075578
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