IUS R/B(1), 25671

Orbit data source: Space-Track

IUS R/B(1), 25671 is space debris in HEO originally from a launch on Fri, 09 Apr 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
25671, 1999-017C
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
BOKT/PWCSD
Mission
Spacecraft
Bus & Motor
ORBUS 21, Unknown motor
Mass
1,164 kg wet, 1,164 kg dry
Launch date (UTC)
1999-04-09 (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: 1 week ago

TLE from 1 week ago
0 IUS R/B(1)
1 25671U 99017C   26166.72321972 -.00000099  00000-0  22901-3 0  9997
2 25671  29.1048   1.6208 7218454 281.5512  11.6560  2.29323143 59708
Epoch: 2026-06-15T17:21Z
TLE epoch observation values (Epoch: 2026-06-15T17:21:26.183Z)
Latitude
-0.00078°
Longitude
-162.73036°
Altitude
3,770.821 km
Speed
7.883 km/s
True Right ascension
00h 06m 32s
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
23:08:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,452.464 km
Perigee altitude
379.365 km
Semi-major axis
24,294.051 km
Eccentricity
0.72185
Inclination
29.1048°
RAAN
1.6208°
Arg. of periapsis
281.5512°
True anomaly
77.76859°
Mean anomaly
11.656°
Eccentric anomaly
35.91829°
Mean motion
0.57318 °/min
Orbital period
628.07 mins
BSTAR
0.00022901
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