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: 18 hours ago

TLE from 18 hours ago

0 NIMBUS 2 DEB
1 37890U 66040AV  26032.83201598  .00001971  00000-0  31959-2 0  9999
2 37890 100.5069 350.6840 0042906 146.8708 213.5123 13.49232416703249

Epoch: 2026-02-01T19:58Z

TLE epoch observation values (Epoch: 2026-02-01T19:58:06.180Z)

Latitude

-0.00003°

Longitude

-80.87775°

Altitude

1,104.549 km

Speed

7.287 km/s

True Right ascension

23h 22m 44s

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

16:05:16

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,104.397 km

Perigee altitude

1,040.462 km

Semi-major axis

7,450.566 km

Eccentricity

0.00429

Inclination

100.5069°

RAAN

350.684°

Arg. of periapsis

146.8708°

True anomaly

213.24205°

Mean anomaly

213.5123°

Eccentric anomaly

213.37706°

Mean motion

3.37489 °/min

Orbital period

106.67 mins

BSTAR

0.0031959

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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.
8 mins	2026-02-02 19:16:36.256Z	96.002° ESE	2026-02-02 19:20:36.256Z	58.034° ENE	17.203°	2026-02-02 19:24:36.256Z	18.76° NNE
11 mins	2026-02-02 20:59:36.256Z	166.17° S	2026-02-02 21:04:36.256Z	197.129° SSW	44.329°	2026-02-02 21:10:36.256Z	342.073° N
12 mins	2026-02-03 09:55:36.256Z	18.66° NNE	2026-02-03 10:01:36.256Z	80.972° E	44.215°	2026-02-03 10:07:36.256Z	191.39° SSW
6 mins	2026-02-03 11:43:36.256Z	331.427° NNW	2026-02-03 11:46:36.256Z	298.331° NW	17.549°	2026-02-03 11:49:36.256Z	267.684° 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, 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: 18 hours ago

TLE from 18 hours ago

TLE epoch observation values (Epoch: 2026-02-01T19:58:06.180Z)

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: 18 hours ago