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: 13 hours ago

TLE from 13 hours ago
0 IUS R/B(2)
1 25869U 99040D   25302.20977104 -.00000370  00000-0  00000+0 0  9994
2 25869  29.8592 195.9273 8061372  15.4600 359.2003  0.97237217 93301
Epoch: 2025-10-29T05:02Z
TLE epoch observation values (Epoch: 2025-10-29T05:02:04.217Z)
Latitude
-0.00093°
Longitude
82.73217°
Altitude
2,037.896 km
Speed
9.244 km/s
True Right ascension
13h 04m 08s
True Declination
0° 00' 03"
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
13:16:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
71,359.107 km
Perigee altitude
1,965.836 km
Semi-major axis
43,040.609 km
Eccentricity
0.80614
Inclination
29.8592°
RAAN
195.9273°
Arg. of periapsis
15.46°
True anomaly
347.49818°
Mean anomaly
359.2003°
Eccentric anomaly
355.88958°
Mean motion
0.24307 °/min
Orbital period
1,481.07 mins
BSTAR
0
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