IUS R/B(2), 24740

Orbit data source: Space-Track

IUS R/B(2), 24740 is space debris in GEO originally from a launch on Sun, 23 Feb 1997 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
24740, 1997-008D
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
BOKT/PWCSD
Mission
Spacecraft
Bus & Motor
ORBUS 6, Unknown motor
Mass
1,079 kg wet, 1,079 kg dry
Launch date (UTC)
1997-02-23 (29 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

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 IUS R/B(2)
1 24740U 97008D   26098.86776734  .00000073  00000-0  00000-0 0  9994
2 24740  14.6077   4.4971 0023967 196.9363 162.9591  0.99498404 25101
Epoch: 2026-04-08T20:49Z
TLE epoch observation values (Epoch: 2026-04-08T20:49:35.098Z)
Latitude
0.00001°
Longitude
-145.04192°
Altitude
36,101.947 km
Speed
3.06 km/s
True Right ascension
00h 17m 54s
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
16:39:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,107.352 km
Perigee altitude
35,904.189 km
Semi-major axis
42,383.908 km
Eccentricity
0.0024
Inclination
14.6077°
RAAN
4.4971°
Arg. of periapsis
196.9363°
True anomaly
163.03935°
Mean anomaly
162.9591°
Eccentric anomaly
162.99925°
Mean motion
0.24874 °/min
Orbital period
1,447.31 mins
BSTAR
0
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Other satellites on launch #8 in the year 1997 (1997-02-23 UTC)

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