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.
Focus sentinelFocus sentinel
Request partner network tasking
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
22315 intel report (Beta)
Focus sentinelFocus sentinel
Edit Public Description
Focus sentinelFocus sentinel
Create New Watchlist
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 IUS R/B(1)
1 22315U 93003C 26084.21749527 .00004110 00000-0 67189-3 0 9995
2 22315 27.0133 322.9954 6020788 302.9239 12.9334 4.02073812179987Epoch: 2026-03-25T05:13Z
TLE epoch observation values (Epoch: 2026-03-25T05:13:11.591Z)
Latitude
0.00044°
Longitude
62.03256°
Altitude
1,659.909 km
Speed
8.679 km/s
True Right ascension
21h 32m 03s
True Declination
0° 00' 02"
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
16:47:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,391.456 km
Perigee altitude
270.842 km
Semi-major axis
16,709.286 km
Eccentricity
0.60208
Inclination
27.0133°
RAAN
322.9954°
Arg. of periapsis
302.9239°
True anomaly
57.1597°
Mean anomaly
12.9334°
Eccentric anomaly
30.37884°
Mean motion
1.00486 °/min
Orbital period
358.26 mins
BSTAR
0.00067189
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #3 in the year 1993 (1993-01-13 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IUS R/B(1) Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 171 mins | 2026-03-27 16:58:18.901Z | 179.886° S | 2026-03-27 17:14:18.901Z | 121.888° SE | 28.657° | 2026-03-27 19:49:18.901Z | 82.242° E |
| 283 mins | 2026-03-27 23:18:18.901Z | 266.498° W | 2026-03-28 01:12:18.901Z | 225.77° WSW | 41.433° | 2026-03-28 04:01:18.901Z | 158.377° S |
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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
|---|