NIMBUS 2 DEB, 37890

Orbit data source: Space-Track

NIMBUS 2 DEB, 37890 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/37890?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

37890, 1966-040AV

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: 10 hours ago

TLE from 10 hours ago

0 NIMBUS 2 DEB
1 37890U 66040AV  26079.39621628  .00002014  00000-0  32432-2 0  9997
2 37890 100.5047  39.6811 0051860  35.3013 325.1535 13.49457892709528

Epoch: 2026-03-20T09:30Z

TLE epoch observation values (Epoch: 2026-03-20T09:30:33.086Z)

Latitude

-0.00001°

Longitude

79.11136°

Altitude

1,045.352 km

Speed

7.345 km/s

True Right ascension

02h 38m 43s

True Declination

0° 00' 00"

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

00:20:52

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,110.233 km

Perigee altitude

1,032.964 km

Semi-major axis

7,449.736 km

Eccentricity

0.00519

Inclination

100.5047°

RAAN

39.6811°

Arg. of periapsis

35.3013°

True anomaly

324.81213°

Mean anomaly

325.1535°

Eccentric anomaly

324.983°

Mean motion

3.37545 °/min

Orbital period

106.65 mins

BSTAR

0.0032432

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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.
10 mins	2026-03-20 20:18:59.048Z	128.774° SE	2026-03-20 20:23:59.048Z	65.868° ENE	32.755°	2026-03-20 20:28:59.048Z	2.333° NNE
9 mins	2026-03-20 22:04:59.048Z	208.034° SW	2026-03-20 22:08:59.048Z	259.568° W	28.567°	2026-03-20 22:13:59.048Z	320.782° NNW
9 mins	2026-03-21 09:15:59.048Z	45.519° ENE	2026-03-21 09:19:59.048Z	93.35° ESE	27.091°	2026-03-21 09:24:59.048Z	152.105° SSE
10 mins	2026-03-21 11:00:59.048Z	356.542° N	2026-03-21 11:04:59.048Z	303.915° NW	35.223°	2026-03-21 11:10:59.048Z	225.583° WSW

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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, 37890 on other resources

View NIMBUS 2 DEB, 37890 on Heavens-Above

View NIMBUS 2 DEB, 37890 on Keep Track

View NIMBUS 2 DEB, 37890 on Celestrak

View NIMBUS 2 DEB, 37890 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, 37890

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-03-20T09:30:33.086Z)

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, 37890 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago