TOS R/B, 22797

Orbit data source: Space-Track

TOS R/B, 22797 is space debris in HEO originally from an American launch on Sun, 12 Sep 1993 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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TOS R/B details

Identifier	22797, 1993-058D
Orbit	HEO
Last TLE update	15 hours ago
Origin	MSFC/OSCD (US)
Manufacturer	MMA/CSD
Mission	Spacecraft
Bus & Motor	ORBUS 21, Unknown motor
Mass	9,366 kg wet, 1,195 kg dry
Launch date (UTC)	1993-09-12 (31 years ago)
Launch vehicle	Unknown
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl + Cone, 3.3 m
Radar Cross Section	8.215 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 15 hours ago

0 TOS R/B
1 22797U 93058D   24361.38718456  .00000943  00000-0  15898-2 0  9999
2 22797  14.8526 263.4321 7363762  75.9322 349.6030  2.12651289236921

Epoch: 2024-12-26T09:17Z

Definitive object data (Epoch: 2024-12-26T09:17:32.745Z)

Latitude	-0.00001°
Longitude	28.8769°
Altitude	3,539.55 km
Speed	8.048 km/s
True Right ascension	17h 34m 31s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-12.47333°
Longitude	-94.98149°
Altitude	32,185.959 km
Speed	2.251 km/s
Apparent Right ascension	09h 33m 49s
Apparent Declination	-16° 29' 54"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	23:32:14
Azimuth	56.195° ENE
Elevation	-55.25°
Doppler factor	1

Orbital elements

Apogee altitude	37,984.693 km
Perigee altitude	357.211 km
Semi-major axis	25,549.089 km
Eccentricity	0.7363762
Inclination	14.8526°
RAAN	263.4321°
Arg. of periapsis	75.9322°
True anomaly	283.80634°
Mean anomaly	349.603°
Eccentric anomaly	326.02556°
Mean motion	0.53147 °/min
BSTAR	0.0015898
Orbital period	677.36 mins