NIMBUS 2 DEB, 31142

Orbit data source: Space-Track

NIMBUS 2 DEB, 31142 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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Iframe URL

https://www.satcat.com/sats-embedded/31142?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

31142, 1966-040AQ

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: 3 hours ago

TLE from 3 hours ago

0 NIMBUS 2 DEB
1 31142U 66040AQ  25336.52939630  .00002234  00000-0  35405-2 0  9993
2 31142 100.6072 342.4503 0058589 287.3477 224.9491 13.50218571916328

Epoch: 2025-12-02T12:42Z

TLE epoch observation values (Epoch: 2025-12-02T12:42:19.840Z)

Latitude

27.69312°

Longitude

-94.13367°

Altitude

1,105.729 km

Speed

7.287 km/s

True Right ascension

11h 12m 14s

True Declination

27° 33' 30"

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

13:47:58

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,112.435 km

Perigee altitude

1,025.173 km

Semi-major axis

7,446.941 km

Eccentricity

0.00586

Inclination

100.6072°

RAAN

342.4503°

Arg. of periapsis

287.3477°

True anomaly

224.47724°

Mean anomaly

224.9491°

Eccentric anomaly

224.71292°

Mean motion

3.37735 °/min

Orbital period

106.59 mins

BSTAR

0.0035405

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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.
8 mins	2025-12-02 22:47:26.501Z	97.28° ESE	2025-12-02 22:51:26.501Z	58.914° ENE	18.178°	2025-12-02 22:55:26.501Z	18.917° NNE
12 mins	2025-12-03 00:30:26.501Z	167.861° S	2025-12-03 00:35:26.501Z	209.031° SW	44.126°	2025-12-03 00:42:26.501Z	341.84° N
11 mins	2025-12-03 13:27:26.501Z	19.502° NNE	2025-12-03 13:32:26.501Z	94.344° ESE	44.587°	2025-12-03 13:38:26.501Z	192.76° SSW
7 mins	2025-12-03 15:13:26.501Z	337.126° NNW	2025-12-03 15:16:26.501Z	306.934° NW	18.357°	2025-12-03 15:20:26.501Z	266.62° W

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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, 31142 on other resources

View NIMBUS 2 DEB, 31142 on Heavens-Above

View NIMBUS 2 DEB, 31142 on Keep Track

View NIMBUS 2 DEB, 31142 on Celestrak

View NIMBUS 2 DEB, 31142 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, 31142

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 hours ago

TLE from 3 hours ago

TLE epoch observation values (Epoch: 2025-12-02T12:42:19.840Z)

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, 31142 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 hours ago