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: 18 hours ago

TLE from 18 hours ago
0 DELTA 1 DEB *
1  5987U 67001S   26037.58851053  .00000523  00000-0  21322-2 0  9998
2  5987  26.3022 200.5583 6704484 196.6842 120.6787  2.89058110374984
Epoch: 2026-02-06T14:07Z
TLE epoch observation values (Epoch: 2026-02-06T14:07:27.309Z)
Latitude
Longitude
-148.05781°
Altitude
25,653.804 km
Speed
2.396 km/s
True Right ascension
13h 22m 07s
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
10:10:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
28,401.201 km
Perigee altitude
483.246 km
Semi-major axis
20,820.36 km
Eccentricity
0.67045
Inclination
26.3022°
RAAN
200.5583°
Arg. of periapsis
196.6842°
True anomaly
163.34377°
Mean anomaly
120.6787°
Eccentric anomaly
143.51829°
Mean motion
0.72246 °/min
Orbital period
498.3 mins
BSTAR
0.0021322
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