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.

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Identifier
22196, 1992-070D
Orbit
LEO
Last TLE update
19 hours ago
Origin
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)

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TLE from 19 hours ago
0 IRIS R/B
1 22196U 92070D   25213.86944382  .00176777  11042-4  98949-3 0  9994
2 22196  41.1049 202.9031 0478088 331.7304  25.8302 14.98105432345632
Epoch: 2025-08-01T20:51Z
TLE epoch observation values (Epoch: 2025-08-01T20:51:59.946Z)
Latitude
-0.00001°
Longitude
-60.81046°
Altitude
276.483 km
Speed
7.906 km/s
True Right ascension
13h 31m 36s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
5.9013°
Longitude
-58.52655°
Altitude
285.017 km
Speed
7.896 km/s
Apparent Right ascension
15h 25m 20s
Apparent Declination
-18° 56' 04"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
05:51:44
Azimuth
67.088° ENE
Elevation
-52.244°
Doppler factor
1
Orbital elements
Apogee altitude
907.412 km
Perigee altitude
242.57 km
Semi-major axis
6,953.128 km
Eccentricity
0.04781
Inclination
41.1049°
RAAN
202.9031°
Arg. of periapsis
331.7304°
True anomaly
28.35175°
Mean anomaly
25.8302°
Eccentric anomaly
27.07707°
Mean motion
3.74346 °/min
Orbital period
96.17 mins
BSTAR
0.00098949
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