IUS R/B(2), 25869

Orbit data source: Space-Track

IUS R/B(2), 25869 is space debris in HEO 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
25869, 1999-040D
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
PW CSD
Mission
Spacecraft
Bus & Motor
ORBUS 6, ORBUS 6
Mass
1,079 kg wet, 1,079 kg dry
Launch date (UTC)
1999-07-23 (26 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.4 m
Radar Cross Section
8.086 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 IUS R/B(2)
1 25869U 99040D   25359.80098245  .00000077  00000-0  00000-0 0  9996
2 25869  29.3908 190.1301 8105397  24.5238 358.6928  0.97237667 93869
Epoch: 2025-12-25T19:13Z
TLE epoch observation values (Epoch: 2025-12-25T19:13:24.883Z)
Latitude
-0.00003°
Longitude
167.05623°
Altitude
2,151.648 km
Speed
9.176 km/s
True Right ascension
12h 39m 50s
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
23:03:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
71,548.626 km
Perigee altitude
1,776.353 km
Semi-major axis
43,040.627 km
Eccentricity
0.81054
Inclination
29.3908°
RAAN
190.1301°
Arg. of periapsis
24.5238°
True anomaly
339.09491°
Mean anomaly
358.6928°
Eccentric anomaly
353.16957°
Mean motion
0.24307 °/min
Orbital period
1,481.08 mins
BSTAR
0
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