NIMBUS 2 DEB, 37888

Orbit data source: Space-Track

NIMBUS 2 DEB, 37888 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/37888?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

37888, 1966-040AT

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

Medium (>0.1 m² and <1 m²)

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

TLE from 2 days ago

0 NIMBUS 2 DEB
1 37888U 66040AT  26155.06279872  .00001941  00000-0  31052-2 0  9998
2 37888 100.5967 190.2754 0043091 253.2785 162.2263 13.50131760834342

Epoch: 2026-06-04T01:30Z

TLE epoch observation values (Epoch: 2026-06-04T01:30:25.809Z)

Latitude

54.34793°

Longitude

-99.88403°

Altitude

1,111.192 km

Speed

7.287 km/s

True Right ascension

11h 40m 56s

True Declination

54° 11' 33"

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

02:59:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,101.214 km

Perigee altitude

1,037.032 km

Semi-major axis

7,447.26 km

Eccentricity

0.00431

Inclination

100.5967°

RAAN

190.2754°

Arg. of periapsis

253.2785°

True anomaly

162.37626°

Mean anomaly

162.2263°

Eccentric anomaly

162.30136°

Mean motion

3.37713 °/min

Orbital period

106.6 mins

BSTAR

0.0031052

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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.
10 mins	2026-06-06 01:23:53.342Z	123.845° SE	2026-06-06 01:27:53.342Z	69.991° E	33.508°	2026-06-06 01:33:53.342Z	359.267° N
10 mins	2026-06-06 03:08:53.342Z	207.516° SW	2026-06-06 03:12:53.342Z	257.677° W	29.604°	2026-06-06 03:18:53.342Z	324.906° NNW
9 mins	2026-06-06 14:19:53.342Z	44.947° NE	2026-06-06 14:23:53.342Z	91.184° ESE	26.632°	2026-06-06 14:28:53.342Z	150.998° SSE
10 mins	2026-06-06 16:04:53.342Z	357.39° N	2026-06-06 16:08:53.342Z	306.248° NW	35.446°	2026-06-06 16:14:53.342Z	225.375° 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, 37888 on other resources

View NIMBUS 2 DEB, 37888 on Heavens-Above

View NIMBUS 2 DEB, 37888 on Keep Track

View NIMBUS 2 DEB, 37888 on Celestrak

View NIMBUS 2 DEB, 37888 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, 37888

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: 2026-06-04T01:30:25.809Z)

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, 37888 on other resources

Documentation

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