IUS R/B(1), 25868

Orbit data source: Space-Track

IUS R/B(1), 25868 is space debris originally from a launch on Fri, 23 Jul 1999 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
25868, 1999-040C
Orbit
Active
Country
Flag of USUS
Related business
Manufacturer
PW CSD
Mission
Spacecraft
Bus & Motor
ORBUS 21, ORBUS 21
Mass
1,164 kg wet, 1,164 kg dry
Launch date (UTC)
1999-07-23 (27 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
8.491 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 IUS R/B(1)
1 25868U 99040C   26085.35685787  .00022058  00000-0  94577-3 0  9993
2 25868  28.4503 175.1683 4347522  30.4912 348.8815  6.84202564607962
Epoch: 2026-03-26T08:33Z
TLE epoch observation values (Epoch: 2026-03-26T08:33:52.519Z)
Latitude
0.00001°
Longitude
-137.10748°
Altitude
534.453 km
Speed
9.018 km/s
True Right ascension
11h 40m 40s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
04:09:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
10,442.727 km
Perigee altitude
248.761 km
Semi-major axis
11,723.881 km
Eccentricity
0.43475
Inclination
28.4503°
RAAN
175.1683°
Arg. of periapsis
30.4912°
True anomaly
329.55168°
Mean anomaly
348.8815°
Eccentric anomaly
340.61279°
Mean motion
1.70976 °/min
Orbital period
210.56 mins
BSTAR
0.00094577
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