IUS R/B(2), 22316

Orbit data source: Space-Track

IUS R/B(2), 22316 is space debris in GEO originally from a launch on Wed, 13 Jan 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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Identifier
22316, 1993-003D
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
UTC CSD
Mission
Spacecraft
Bus & Motor
ORBUS 6, Unknown motor
Mass
~1,100 kg wet, ~1,100 kg dry
Launch date (UTC)
1993-01-13 (34 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.8 m
Radar Cross Section
8.086 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 4 weeks ago

TLE from 4 weeks ago
0 IUS R/B(2)
1 22316U 93003D   26240.23799618 -.00000224  00000-0  00000-0 0  9997
2 22316  11.8165 344.1054 0067666 127.0712 231.0267  1.00102722127905
Epoch: 2026-08-28T05:42Z
TLE epoch observation values (Epoch: 2026-08-28T05:42:42.869Z)
Latitude
-0.52669°
Longitude
-80.49937°
Altitude
36,015.966 km
Speed
3.06 km/s
True Right ascension
22h 46m 34s
True Declination
0° 31' 34"
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
07:01:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,120.7 km
Perigee altitude
35,549.42 km
Semi-major axis
42,213.197 km
Eccentricity
0.00677
Inclination
11.8165°
RAAN
344.1054°
Arg. of periapsis
127.0712°
True anomaly
230.42708°
Mean anomaly
231.0267°
Eccentric anomaly
230.72657°
Mean motion
0.25025 °/min
Orbital period
1,438.57 mins
BSTAR
0
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Other satellites on launch #3 in the year 1993 (1993-01-13 UTC)

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