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: 14 hours ago

TLE from 14 hours ago

0 NIMBUS 2 DEB
1 31142U 66040AQ  26032.99969517  .00001532  00000-0  24419-2 0  9998
2 31142 100.6067  47.8645 0057266 141.3769 247.7729 13.50487819924621

Epoch: 2026-02-01T23:59Z

TLE epoch observation values (Epoch: 2026-02-01T23:59:33.662Z)

Latitude

28.05572°

Longitude

-89.92551°

Altitude

1,090.119 km

Speed

7.302 km/s

True Right ascension

02h 48m 39s

True Declination

27° 55' 10"

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

16:09:06

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,110.454 km

Perigee altitude

1,025.174 km

Semi-major axis

7,445.951 km

Eccentricity

0.00573

Inclination

100.6067°

RAAN

47.8645°

Arg. of periapsis

141.3769°

True anomaly

247.16709°

Mean anomaly

247.7729°

Eccentric anomaly

247.46983°

Mean motion

3.37803 °/min

Orbital period

106.57 mins

BSTAR

0.0024419

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

THOR AGENA B R/B, 2174

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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.
11 mins	2026-02-02 14:39:25.151Z	0.026° NNE	2026-02-02 14:44:25.151Z	301.898° NW	33.432°	2026-02-02 14:50:25.151Z	227.051° WSW
7 mins	2026-02-02 23:09:25.151Z	87.877° E	2026-02-02 23:12:25.151Z	55.806° ENE	18.116°	2026-02-02 23:16:25.151Z	16.52° NNE
11 mins	2026-02-03 00:51:25.151Z	169.056° S	2026-02-03 00:56:25.151Z	236.805° WSW	44.346°	2026-02-03 01:02:25.151Z	340.822° N
11 mins	2026-02-03 13:47:25.151Z	18.987° NNE	2026-02-03 13:52:25.151Z	81.853° E	44.541°	2026-02-03 13:58:25.151Z	193.099° 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, 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: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-02-01T23:59:33.662Z)

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: 14 hours ago