NIMBUS 2 DEB, 37889

Orbit data source: Space-Track

NIMBUS 2 DEB, 37889 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/37889?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

37889, 1966-040AU

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 weeks ago

TLE from 3 weeks ago

0 NIMBUS 2 DEB
1 37889U 66040AU  25316.20225878  .00003061  00000-0  46806-2 0  9998
2 37889 100.5544 315.4815 0063752 338.9969  94.3127 13.51950307782796

Epoch: 2025-11-12T04:51Z

TLE epoch observation values (Epoch: 2025-11-12T04:51:15.158Z)

Latitude

71.0145°

Longitude

158.48977°

Altitude

1,081.117 km

Speed

7.316 km/s

True Right ascension

18h 51m 31s

True Declination

70° 54' 47"

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

06:57:32

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,109.871 km

Perigee altitude

1,015.001 km

Semi-major axis

7,440.573 km

Eccentricity

0.00638

Inclination

100.5544°

RAAN

315.4815°

Arg. of periapsis

338.9969°

True anomaly

95.04072°

Mean anomaly

94.3127°

Eccentric anomaly

94.67676°

Mean motion

3.38169 °/min

Orbital period

106.46 mins

BSTAR

0.0046806

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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.
12 mins	2025-12-01 12:38:03.998Z	28.444° NE	2025-12-01 12:44:03.998Z	110.942° ESE	37.994°	2025-12-01 12:50:03.998Z	176.555° S
9 mins	2025-12-01 14:24:03.998Z	347.202° N	2025-12-01 14:28:03.998Z	301.698° NW	26.046°	2025-12-01 14:33:03.998Z	246.113° WSW
9 mins	2025-12-01 22:51:03.998Z	105.74° ESE	2025-12-01 22:55:03.998Z	56.123° ENE	25.25°	2025-12-01 23:00:03.998Z	6.152° NNE
11 mins	2025-12-02 00:34:03.998Z	186.248° SSW	2025-12-02 00:39:03.998Z	252.76° W	38.24°	2025-12-02 00:45:03.998Z	332.493° NNW

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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, 37889 on other resources

View NIMBUS 2 DEB, 37889 on Heavens-Above

View NIMBUS 2 DEB, 37889 on Keep Track

View NIMBUS 2 DEB, 37889 on Celestrak

View NIMBUS 2 DEB, 37889 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, 37889

Orbit data source: Space-Track

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

TLE from 3 weeks ago

TLE epoch observation values (Epoch: 2025-11-12T04:51:15.158Z)

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, 37889 on other resources

Documentation

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