IABS R/B, 26577
Orbit data source: Space-Track
IABS R/B, 26577 is space debris in GEO originally from a launch on Fri, 20 Oct 2000 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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26577 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
LMEW/PRIMVN
Mission
Spacecraft
Bus & Motor
IABS, R-4D-11-164X2
Mass
270 kg wet, 270 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.4 m
Radar Cross Section
4.897 m²
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 IABS R/B
1 26577U 00065C 25240.84523965 -.00000302 00000-0 00000-0 0 9999
2 26577 13.8868 3.8196 0056548 269.2504 90.1397 1.01186516 23267Epoch: 2025-08-28T20:17Z
TLE epoch observation values (Epoch: 2025-08-28T20:17:08.705Z)
Latitude
0.00002°
Longitude
82.25259°
Altitude
35,532.649 km
Speed
3.084 km/s
True Right ascension
00h 15m 21s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
13:17:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,770.082 km
Perigee altitude
35,296.083 km
Semi-major axis
41,911.219 km
Eccentricity
0.00565
Inclination
13.8868°
RAAN
3.8196°
Arg. of periapsis
269.2504°
True anomaly
90.78767°
Mean anomaly
90.1397°
Eccentric anomaly
90.46369°
Mean motion
0.25296 °/min
Orbital period
1,423.16 mins
BSTAR
0
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Other satellites on launch #65 in the year 2000 (2000-10-20 UTC)
IABS R/B Visibility
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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26577 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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