IABS R/B, 22916
Orbit data source: Space-Track
IABS R/B, 22916 is space debris in GEO originally from a launch on Sun, 28 Nov 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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22916 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
MM/Valley Forge
Mission
Spacecraft
Bus & Motor
R-4D, R-4D-12 X2
Mass
270 kg wet, 270 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.4 m
Radar Cross Section
4.851 m²
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 IABS R/B
1 22916U 93074B 25351.95985627 -.00000158 00000-0 00000-0 0 9995
2 22916 13.9154 343.3735 0057900 99.7209 260.9318 0.99981651 24092Epoch: 2025-12-17T23:02Z
TLE epoch observation values (Epoch: 2025-12-17T23:02:11.581Z)
Latitude
0.00001°
Longitude
-89.01758°
Altitude
35,907.791 km
Speed
3.069 km/s
True Right ascension
22h 53m 24s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
13:57:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,113.716 km
Perigee altitude
35,624.493 km
Semi-major axis
42,247.242 km
Eccentricity
0.00579
Inclination
13.9154°
RAAN
343.3735°
Arg. of periapsis
99.7209°
True anomaly
260.27737°
Mean anomaly
260.9318°
Eccentric anomaly
260.60451°
Mean motion
0.24995 °/min
Orbital period
1,440.31 mins
BSTAR
0
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Other satellites on launch #74 in the year 1993 (1993-11-28 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IABS R/B Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-12-19 15:03:48.611Z | 162.102° S | 2025-12-20 04:46:48.611Z | 150.49° SSE | 39.779° | 2025-12-20 15:03:48.611Z | 163.337° S |
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22916 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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