DELTA 1 DEB, 26842

Orbit data source: Space-Track

DELTA 1 DEB, 26842 is space debris in SSO originally from a launch on Thu, 12 Jun 1975 UTC launched from the Air Force Western Test Range (AFWTR). 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
26842, 1975-052KW
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1975-06-12 (51 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.050 m
Radar Cross Section
Small (<0.1 m²)

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

TLE from 3 days ago
0 DELTA 1 DEB
1 26842U 75052KW  26300.24477941  .00000718  00000-0  75063-3 0  9990
2 26842  99.8394 297.9500 0038520 303.6000  69.8443 13.78669609435582
Epoch: 2026-10-27T05:52Z
TLE epoch observation values (Epoch: 2026-10-27T05:52:28.941Z)
Latitude
13.62014°
Longitude
171.82279°
Altitude
961.034 km
Speed
7.377 km/s
True Right ascension
19h 42m 12s
True Declination
13° 32' 38"
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
13:39:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
994.169 km
Perigee altitude
937.591 km
Semi-major axis
7,344.017 km
Eccentricity
0.00385
Inclination
99.8394°
RAAN
297.95°
Arg. of periapsis
303.6°
True anomaly
70.25936°
Mean anomaly
69.8443°
Eccentric anomaly
70.05176°
Mean motion
3.4486 °/min
Orbital period
104.39 mins
BSTAR
0.00075063
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