IUS R/B(1), 24739

Orbit data source: Space-Track

IUS R/B(1), 24739 is space debris in HEO 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
24739, 1997-008C
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)
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, Unknown HBR
Radar Cross Section
7.708 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 IUS R/B(1)
1 24739U 97008C   26099.53461717  .00000192  00000-0  34591-3 0  9996
2 24739  28.3241 297.1676 7130651 318.8558   5.0895  2.41397848 61129
Epoch: 2026-04-09T12:49Z
TLE epoch observation values (Epoch: 2026-04-09T12:49:50.923Z)
Latitude
0.00094°
Longitude
-93.05869°
Altitude
1,147.752 km
Speed
9.431 km/s
True Right ascension
19h 48m 44s
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
14:57:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,839.859 km
Perigee altitude
358.295 km
Semi-major axis
23,477.214 km
Eccentricity
0.71307
Inclination
28.3241°
RAAN
297.1676°
Arg. of periapsis
318.8558°
True anomaly
40.36021°
Mean anomaly
5.0895°
Eccentric anomaly
17.10848°
Mean motion
0.60336 °/min
Orbital period
596.66 mins
BSTAR
0.00034591
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Other satellites on launch #8 in the year 1997 (1997-02-23 UTC)

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