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: 1 day ago

TLE from 1 day ago

0 NIMBUS 2 DEB
1 37890U 66040AV  26129.88152413  .00001552  00000-0  25145-2 0  9997
2 37890 100.5003  92.8141 0044509 281.0578  78.5550 13.49671297716335

Epoch: 2026-05-09T21:09Z

TLE epoch observation values (Epoch: 2026-05-09T21:09:23.684Z)

Latitude

0.00001°

Longitude

-92.22718°

Altitude

1,069.784 km

Speed

7.32 km/s

True Right ascension

06h 11m 15s

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

06:58:18

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,103.967 km

Perigee altitude

1,037.658 km

Semi-major axis

7,448.95 km

Eccentricity

0.00445

Inclination

100.5003°

RAAN

92.8141°

Arg. of periapsis

281.0578°

True anomaly

79.05544°

Mean anomaly

78.555°

Eccentric anomaly

78.80517°

Mean motion

3.37599 °/min

Orbital period

106.64 mins

BSTAR

0.0025145

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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	2026-05-11 09:21:49.056Z	43.764° NE	2026-05-11 09:26:49.056Z	98.914° ESE	24.684°	2026-05-11 09:31:49.056Z	150.55° SSE
11 mins	2026-05-11 11:06:49.056Z	1.83° NNE	2026-05-11 11:11:49.056Z	294.574° NW	38.051°	2026-05-11 11:17:49.056Z	220.19° SW
6 mins	2026-05-11 19:36:49.056Z	81.371° E	2026-05-11 19:39:49.056Z	51.55° ENE	15.583°	2026-05-11 19:42:49.056Z	23.264° NE
11 mins	2026-05-11 21:18:49.056Z	160.654° S	2026-05-11 21:23:49.056Z	15.689° NNE	44.877°	2026-05-11 21:29:49.056Z	344.995° N

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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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-05-09T21:09:23.684Z)

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: 1 day ago