IUS R/B(1), 22315

Orbit data source: Space-Track

IUS R/B(1), 22315 is space debris in HEO 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
22315, 1993-003C
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
UTC CSD
Mission
Spacecraft
Bus & Motor
ORBUS 21, Unknown motor
Mass
1,164 kg wet, ~1,164 kg dry
Launch date (UTC)
1993-01-13 (33 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, Unknown HBR
Radar Cross Section
7.708 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 IUS R/B(1)
1 22315U 93003C   25348.74130118  .00006682  00000-0  89683-3 0  9994
2 22315  26.9693  38.3163 6034891 177.4365 188.2716  4.00983185175945
Epoch: 2025-12-14T17:47Z
TLE epoch observation values (Epoch: 2025-12-14T17:47:28.421Z)
Latitude
0.00002°
Longitude
47.79979°
Altitude
20,415.567 km
Speed
2.437 km/s
True Right ascension
02h 33m 16s
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
13:26:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,463.592 km
Perigee altitude
259.288 km
Semi-major axis
16,739.577 km
Eccentricity
0.60349
Inclination
26.9693°
RAAN
38.3163°
Arg. of periapsis
177.4365°
True anomaly
182.56779°
Mean anomaly
188.2716°
Eccentric anomaly
185.16113°
Mean motion
1.00214 °/min
Orbital period
359.23 mins
BSTAR
0.00089683
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Other satellites on launch #3 in the year 1993 (1993-01-13 UTC)

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