NIMBUS 2 DEB, 40642

Orbit data source: Space-Track

NIMBUS 2 DEB, 40642 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/40642?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40642, 1966-040BF

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 week ago

TLE from 1 week ago

0 NIMBUS 2 DEB
1 40642U 66040BF  26255.71746893  .00003375  00000-0  44693-2 0  9993
2 40642 100.3137 174.4821 0035235 198.9748 161.0080 13.61364324557336

Epoch: 2026-09-12T17:13Z

TLE epoch observation values (Epoch: 2026-09-12T17:13:09.315Z)

Latitude

0.00001°

Longitude

-75.52918°

Altitude

1,058.216 km

Speed

7.311 km/s

True Right ascension

11h 37m 55s

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

19:19:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,054.152 km

Perigee altitude

1,001.961 km

Semi-major axis

7,406.194 km

Eccentricity

0.00352

Inclination

100.3137°

RAAN

174.4821°

Arg. of periapsis

198.9748°

True anomaly

161.13885°

Mean anomaly

161.008°

Eccentric anomaly

161.07348°

Mean motion

3.40526 °/min

Orbital period

105.72 mins

BSTAR

0.0044693

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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	2026-09-20 07:28:51.893Z	20.401° NNE	2026-09-20 07:34:51.893Z	119.082° SE	71.093°	2026-09-20 07:40:51.893Z	188.685° SSW
6 mins	2026-09-20 09:15:51.893Z	329.116° NNW	2026-09-20 09:17:51.893Z	306.282° NW	19.578°	2026-09-20 09:21:51.893Z	262.985° W
10 mins	2026-09-20 17:36:51.893Z	121.414° SE	2026-09-20 17:41:51.893Z	58.375° ENE	34.472°	2026-09-20 17:46:51.893Z	3.677° NNE
10 mins	2026-09-20 19:20:51.893Z	197.891° SSW	2026-09-20 19:25:51.893Z	266.237° W	40.084°	2026-09-20 19:30:51.893Z	326.119° 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, 40642 on other resources

View NIMBUS 2 DEB, 40642 on Heavens-Above

View NIMBUS 2 DEB, 40642 on Keep Track

View NIMBUS 2 DEB, 40642 on Celestrak

View NIMBUS 2 DEB, 40642 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, 40642

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 week ago

TLE from 1 week ago

TLE epoch observation values (Epoch: 2026-09-12T17:13:09.315Z)

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, 40642 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 week ago