IRIS R/B, 22196

Orbit data source: Space-Track

IRIS R/B, 22196 is space debris in LEO originally from a launch on Thu, 22 Oct 1992 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.

Not visible in the next 10 days
Identifier
22196, 1992-070D
Orbit
LEO
Country
Flag of ITIT
Related business
Manufacturer
BPD
Mission
Spacecraft
Bus & Motor
IRIS, Unknown motor
Mass
1,534 kg wet, 264 kg dry
Launch date (UTC)
1992-10-22 (33 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + Cone, 0.8 m
Radar Cross Section
2.399 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 22 hours ago

TLE from 22 hours ago
0 IRIS R/B
1 22196U 92070D   25284.07835146  .00300042  26262-4  11576-2 0  9996
2 22196  41.0944 161.4988 0346190 101.6563 262.3319 15.32200166356271
Epoch: 2025-10-11T01:52Z
TLE epoch observation values (Epoch: 2025-10-11T01:52:49.566Z)
Latitude
-0.00003°
Longitude
113.37724°
Altitude
508.435 km
Speed
7.59 km/s
True Right ascension
10h 45m 59s
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
18:02:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
708.65 km
Perigee altitude
234.394 km
Semi-major axis
6,849.659 km
Eccentricity
0.03462
Inclination
41.0944°
RAAN
161.4988°
Arg. of periapsis
101.6563°
True anomaly
258.42593°
Mean anomaly
262.3319°
Eccentric anomaly
260.37629°
Mean motion
3.8286 °/min
Orbital period
94.03 mins
BSTAR
0.0011576
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