Satellite description

CELESTIS 02/TAURUS R/B, 25160 is space debris in LEO originally from a launch on Tue, 10 Feb 1998 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.

Satellite metadata
Identifier
25160, 1998-007D
Orbit
LEO
Last TLE update
8 hours ago
Origin
Flag of USOSCC (US)
Manufacturer
Alliant
Mission
Operational Commercial Misc
Bus & Motor
ORION 38, Unknown motor
Mass
202 kg wet, 202 kg dry
Launch date (UTC)
1998-02-10 (27 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cone + Cyl, 2 m
Radar Cross Section
1.390 m², Large (>1 m²)
Visualization orbit readout
Latitude
25.45798°
Longitude
53.54612°
Altitude
794.805 km
Speed
7.472 km/s
Apparent Right ascension
20h 12m 55s
Apparent Declination
-14° 15' 12"
Sunlit
Object is in full shadow
Orbital elements
Apogee altitude
858.554 km
Perigee altitude
772.042 km
Semi-major axis
7,193.435 km
Eccentricity
0.00601
Inclination
108.004°
RAAN
262.422°
Arg. of periapsis
81.8869°
True anomaly
Unknown
Mean anomaly
27.5859°
Eccentric anomaly
Unknown
Mean motion
3.55745 °/min
Orbital period
101.2 mins
BSTAR
0.00007804
25160, CELESTIS 02/TAURUS R/B
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