DELTA 1 DEB, 13826

Orbit data source: Space-Track

DELTA 1 DEB, 13826 is space debris in SSO originally from a launch on Sun, 05 Mar 1978 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
13826, 1978-026FV
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1978-03-05 (48 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

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

TLE from 2 days ago
0 DELTA 1 DEB
1 13826U 78026FV  26171.31908610  .00005245  00000-0  60390-3 0  9995
2 13826  98.2405 191.2583 0027722  89.3713 271.0677 14.85909751302756
Epoch: 2026-06-20T07:39Z
TLE epoch observation values (Epoch: 2026-06-20T07:39:29.039Z)
Latitude
-0.00005°
Longitude
167.85189°
Altitude
613.444 km
Speed
7.553 km/s
True Right ascension
12h 45m 01s
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
00:39:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.147 km
Perigee altitude
588.414 km
Semi-major axis
6,985.917 km
Eccentricity
0.00277
Inclination
98.2405°
RAAN
191.2583°
Arg. of periapsis
89.3713°
True anomaly
270.75007°
Mean anomaly
271.0677°
Eccentric anomaly
270.90888°
Mean motion
3.71713 °/min
Orbital period
96.85 mins
BSTAR
0.0006039
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