IABS R/B, 22916

Orbit data source: Space-Track

IABS R/B, 22916 is space debris in GEO originally from a launch on Sun, 28 Nov 1993 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

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/22916?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/22916?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

22916, 1993-074B

Orbit

GEO

Last TLE update

1 day ago

Origin

United States Space Force (US)

Manufacturer

MM/Valley Forge

Mission

Spacecraft

Bus & Motor

R-4D, R-4D-12 X2

Mass

270 kg wet, 270 kg dry

Launch date (UTC)

1993-11-28 (32 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 2.9 m

Radar Cross Section

4.851 m²

Expand to show TLE details & history

TLE from 1 day ago

0 IABS R/B
1 22916U 93074B   25188.94947021 -.00000059  00000-0  00000-0 0  9998
2 22916  14.0293 344.5859 0066051  98.4864 262.2888  0.99975261 22464

Epoch: 2025-07-07T22:47Z

TLE epoch observation values (Epoch: 2025-07-07T22:47:14.226Z)

Latitude

0.00002°

Longitude

76.63655°

Altitude

35,909.787 km

Speed

3.069 km/s

True Right ascension

22h 58m 23s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

11.10188°

Longitude

-154.98259°

Altitude

35,622.822 km

Speed

3.09 km/s

Apparent Right ascension

07h 30m 56s

Apparent Declination

4° 58' 06"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

19:22:48

Azimuth

357.131° N

Elevation

-45.076°

Doppler factor

Orbital elements

Apogee altitude

36,149.962 km

Perigee altitude

35,591.844 km

Semi-major axis

42,249.04 km

Eccentricity

0.00661

Inclination

14.0293°

RAAN

344.5859°

Arg. of periapsis

98.4864°

True anomaly

Unknown

Mean anomaly

262.2888°

Eccentric anomaly

Unknown

Mean motion

0.24993 °/min

Orbital period

1,440.4 mins

BSTAR

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22916 neighbors

Authenticating...

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Other satellites on launch #74 in the year 1993 (1993-11-28 UTC)

USA 97, 22915

ATLAS 2 CENTAUR R/B, 22924 (Decayed)

IABS R/B Visibility

Observer location: undefined°, undefined°

IABS R/B is likely not visible in the next few days

Authenticating...

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Check out IABS R/B, 22916 on other resources

View IABS R/B, 22916 on Heavens-Above

View IABS R/B, 22916 on Keep Track

View IABS R/B, 22916 on Celestrak

View IABS R/B, 22916 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.