PEGASUS R/B, 41892

Orbit data source: Space-Track

PEGASUS R/B, 41892 is space debris in LEO originally from a launch on Thu, 15 Dec 2016 UTC launched from the Pegasus Launch, Eastern Range Air Space (ERAS). 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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<iframe src="https://www.satcat.com/sats-embedded/41892?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/41892?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41892, 2016-078J

Orbit

LEO

Last TLE update

9 hours ago

Origin

Northrop Grumman (US)

Manufacturer

OATK FSG Utah

Mission

Spacecraft

Bus & Motor

ORION 38, Unknown motor

Mass

315 kg wet, 202 kg dry

Launch date (UTC)

2016-12-15 (9 years ago)

Launch vehicle

Unknown

Launch site

Pegasus Launch, Eastern Range Air Space (ERAS)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Nozzle, 1.4 m

Radar Cross Section

1.427 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago

0 PEGASUS R/B
1 41892U 16078J   25183.49047040  .00015515  00000-0  29334-3 0  9994
2 41892  34.9372 341.2901 0008603 137.9086 222.2297 15.47461991475082

Epoch: 2025-07-02T11:46Z

TLE epoch observation values (Epoch: 2025-07-02T11:46:16.642Z)

Latitude

-0.00002°

Longitude

-116.0501°

Altitude

427.377 km

Speed

7.655 km/s

True Right ascension

22h 45m 09s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

22.91679°

Longitude

-81.62891°

Altitude

423.756 km

Speed

7.661 km/s

Apparent Right ascension

23h 17m 21s

Apparent Declination

-8° 28' 35"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

08:58:49

Azimuth

306.049° NW

Elevation

-45.952°

Doppler factor

Orbital elements

Apogee altitude

433.303 km

Perigee altitude

421.594 km

Semi-major axis

6,805.585 km

Eccentricity

0.00086

Inclination

34.9372°

RAAN

341.2901°

Arg. of periapsis

137.9086°

True anomaly

Unknown

Mean anomaly

222.2297°

Eccentric anomaly

Unknown

Mean motion

3.86585 °/min

Orbital period

93.12 mins

BSTAR

0.00029334

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Other satellites on launch #78 in the year 2016 (2016-12-15 UTC)

CYGFM06, 41889 (Decayed)

CYGFM07, 41890

CYGFM03, 41891

PEGASUS R/B Visibility forecast

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.
4 mins	2025-07-03 14:20:39.564Z	200.724° SSW	2025-07-03 14:22:39.564Z	159.657° S	17.551°	2025-07-03 14:24:39.564Z	120.016° SE
4 mins	2025-07-03 15:58:39.564Z	226.155° WSW	2025-07-03 16:00:39.564Z	162.172° S	28.05°	2025-07-03 16:02:39.564Z	116.581° SE
4 mins	2025-07-03 17:36:39.564Z	232.224° WSW	2025-07-03 17:37:39.564Z	206.723° SW	23.846°	2025-07-03 17:40:39.564Z	134.566° SE

Authenticating...

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Check out PEGASUS R/B, 41892 on other resources

View PEGASUS R/B, 41892 on Heavens-Above

View PEGASUS R/B, 41892 on Keep Track

View PEGASUS R/B, 41892 on Celestrak

View PEGASUS R/B, 41892 on Gunter's Space Page

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