NIMBUS 2 DEB, 37892

Orbit data source: Space-Track

NIMBUS 2 DEB, 37892 is space debris in SSO originally from a launch on Sun, 15 May 1966 UTC launched from the Air Force Western Test Range (AFWTR). 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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https://www.satcat.com/sats-embedded/37892?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

37892, 1966-040AX

Orbit

SSO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-05-15 (60 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 NIMBUS 2 DEB
1 37892U 66040AX  25346.81265688  .00002852  00000-0  46992-2 0  9998
2 37892 100.5091 291.4669 0051772 286.0105 102.3252 13.47560610336772

Epoch: 2025-12-12T19:30Z

TLE epoch observation values (Epoch: 2025-12-12T19:30:13.554Z)

Latitude

28.42935°

Longitude

-88.57243°

Altitude

1,093.047 km

Speed

7.304 km/s

True Right ascension

19h 02m 55s

True Declination

28° 17' 31"

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

08:16:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,117.2 km

Perigee altitude

1,039.99 km

Semi-major axis

7,456.732 km

Eccentricity

0.00518

Inclination

100.5091°

RAAN

291.4669°

Arg. of periapsis

286.0105°

True anomaly

102.90398°

Mean anomaly

102.3252°

Eccentric anomaly

102.61467°

Mean motion

3.3707 °/min

Orbital period

106.8 mins

BSTAR

0.0046992

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Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)

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NIMBUS 2 DEB Visibility forecast

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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.
12 mins	2025-12-13 10:11:51.844Z	2.19° NNE	2025-12-13 10:17:51.844Z	290.214° WNW	35.587°	2025-12-13 10:23:51.844Z	224.213° SW
7 mins	2025-12-13 18:42:51.844Z	88.517° E	2025-12-13 18:45:51.844Z	57.975° ENE	17.882°	2025-12-13 18:49:51.844Z	18.759° NNE
12 mins	2025-12-13 20:24:51.844Z	166.871° S	2025-12-13 20:30:51.844Z	305.508° NW	44.265°	2025-12-13 20:36:51.844Z	342.296° N
12 mins	2025-12-14 09:22:51.844Z	18.467° NNE	2025-12-14 09:28:51.844Z	146.152° SSE	44.452°	2025-12-14 09:34:51.844Z	193.426° SSW

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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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out NIMBUS 2 DEB, 37892 on other resources

View NIMBUS 2 DEB, 37892 on Heavens-Above

View NIMBUS 2 DEB, 37892 on Keep Track

View NIMBUS 2 DEB, 37892 on Celestrak

View NIMBUS 2 DEB, 37892 on Gunter's Space Page

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

NIMBUS 2 DEB, 37892

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2025-12-12T19:30:13.554Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)

NIMBUS 2 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out NIMBUS 2 DEB, 37892 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago