NIMBUS 2 DEB, 37893

Orbit data source: Space-Track

NIMBUS 2 DEB, 37893 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/37893?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

37893, 1966-040AY

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: 2 days ago

TLE from 2 days ago

0 NIMBUS 2 DEB
1 37893U 66040AY  26077.15988934  .00001658  00000-0  26877-2 0  9997
2 37893 100.5079  46.5436 0061068  26.0955 355.6883 13.49182901672269

Epoch: 2026-03-18T03:50Z

TLE epoch observation values (Epoch: 2026-03-18T03:50:14.438Z)

Latitude

21.36013°

Longitude

169.11741°

Altitude

1,032.348 km

Speed

7.36 km/s

True Right ascension

02h 49m 37s

True Declination

21° 14' 53"

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

17:27:27

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,118.112 km

Perigee altitude

1,027.112 km

Semi-major axis

7,450.749 km

Eccentricity

0.00611

Inclination

100.5079°

RAAN

46.5436°

Arg. of periapsis

26.0955°

True anomaly

355.63528°

Mean anomaly

355.6883°

Eccentric anomaly

355.66183°

Mean motion

3.37476 °/min

Orbital period

106.67 mins

BSTAR

0.0026877

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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.
6 mins	2026-03-20 19:59:42.188Z	83.785° E	2026-03-20 20:02:42.188Z	53.996° ENE	14.634°	2026-03-20 20:05:42.188Z	24.691° NE
11 mins	2026-03-20 21:41:42.188Z	160.953° S	2026-03-20 21:46:42.188Z	120.525° SE	44.93°	2026-03-20 21:52:42.188Z	344.931° N
11 mins	2026-03-21 10:38:42.188Z	23.603° NE	2026-03-21 10:43:42.188Z	107.573° ESE	43.133°	2026-03-21 10:49:42.188Z	186.86° SSW
8 mins	2026-03-21 12:24:42.188Z	338.71° N	2026-03-21 12:27:42.188Z	306.861° NW	20.394°	2026-03-21 12:32:42.188Z	256.152° 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, 37893 on other resources

View NIMBUS 2 DEB, 37893 on Heavens-Above

View NIMBUS 2 DEB, 37893 on Keep Track

View NIMBUS 2 DEB, 37893 on Celestrak

View NIMBUS 2 DEB, 37893 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, 37893

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-03-18T03:50:14.438Z)

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, 37893 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago