NIMBUS 2 DEB, 40645

Orbit data source: Space-Track

NIMBUS 2 DEB, 40645 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/40645?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40645, 1966-040BJ

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)

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Last TLE update: 3 days ago

TLE from 3 days ago

0 NIMBUS 2 DEB
1 40645U 66040BJ  26030.60141502  .00000994  00000-0  17703-2 0  9997
2 40645 100.4090 266.4960 0038869 158.7926 201.4824 13.44729102524410

Epoch: 2026-01-30T14:26Z

TLE epoch observation values (Epoch: 2026-01-30T14:26:02.257Z)

Latitude

-0.00005°

Longitude

-79.85081°

Altitude

1,121.505 km

Speed

7.279 km/s

True Right ascension

17h 45m 59s

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

17:46:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,118.085 km

Perigee altitude

1,060.036 km

Semi-major axis

7,467.198 km

Eccentricity

0.00389

Inclination

100.409°

RAAN

266.496°

Arg. of periapsis

158.7926°

True anomaly

201.32002°

Mean anomaly

201.4824°

Eccentric anomaly

201.40114°

Mean motion

3.36362 °/min

Orbital period

107.03 mins

BSTAR

0.0017703

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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.
5 mins	2026-02-03 03:02:08.891Z	74.326° E	2026-02-03 03:04:08.891Z	95.092° ESE	14.756°	2026-02-03 03:07:08.891Z	123.643° SE
11 mins	2026-02-03 04:45:08.891Z	12.643° NNE	2026-02-03 04:50:08.891Z	255.906° W	44.526°	2026-02-03 04:56:08.891Z	201.902° SSW
4 mins	2026-02-03 06:33:08.891Z	318.363° NNW	2026-02-03 06:34:08.891Z	308.296° NW	13.855°	2026-02-03 06:37:08.891Z	279.439° WNW
11 mins	2026-02-03 14:59:08.891Z	141.367° SSE	2026-02-03 15:04:08.891Z	68.976° E	40.101°	2026-02-03 15:10:08.891Z	353.556° 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, 40645 on other resources

View NIMBUS 2 DEB, 40645 on Heavens-Above

View NIMBUS 2 DEB, 40645 on Keep Track

View NIMBUS 2 DEB, 40645 on Celestrak

View NIMBUS 2 DEB, 40645 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, 40645

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-01-30T14:26:02.257Z)

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, 40645 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago