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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 4 days ago

TLE from 4 days ago

0 NIMBUS 2 DEB
1 31142U 66040AQ  26170.03084346  .00001111  00000-0  17812-2 0  9996
2 31142 100.6004 193.7608 0054521 166.3108 222.2133 13.50926479943120

Epoch: 2026-06-19T00:44Z

TLE epoch observation values (Epoch: 2026-06-19T00:44:24.874Z)

Latitude

27.62637°

Longitude

-90.20082°

Altitude

1,102.272 km

Speed

7.289 km/s

True Right ascension

12h 32m 40s

True Declination

27° 29' 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

02:14:50

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,106.787 km

Perigee altitude

1,025.613 km

Semi-major axis

7,444.337 km

Eccentricity

0.00545

Inclination

100.6004°

RAAN

193.7608°

Arg. of periapsis

166.3108°

True anomaly

221.79564°

Mean anomaly

222.2133°

Eccentric anomaly

222.00426°

Mean motion

3.37912 °/min

Orbital period

106.54 mins

BSTAR

0.0017812

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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.
7 mins	2026-06-22 16:17:02.458Z	339.65° N	2026-06-22 16:21:02.458Z	298.376° NW	16.822°	2026-06-22 16:24:02.458Z	268.209° W
11 mins	2026-06-23 00:43:02.458Z	130.448° SE	2026-06-23 00:48:02.458Z	63.911° ENE	34.866°	2026-06-23 00:54:02.458Z	357.099° N
9 mins	2026-06-23 02:29:02.458Z	212.263° SW	2026-06-23 02:33:02.458Z	263.495° W	27.882°	2026-06-23 02:38:02.458Z	320.207° NNW
9 mins	2026-06-23 13:39:02.458Z	43.534° NE	2026-06-23 13:43:02.458Z	91.469° ESE	27.108°	2026-06-23 13:48:02.458Z	153.496° SSE

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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: 4 days ago

TLE from 4 days ago

TLE epoch observation values (Epoch: 2026-06-19T00:44:24.874Z)

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: 4 days ago