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)

Expand to show TLE details & history
Last TLE update: 6 days ago

TLE from 6 days ago

0 NIMBUS 2 DEB
1 40645U 66040BJ  26119.94569816  .00001181  00000-0  20758-2 0  9997
2 40645 100.4100 358.9515 0045672 308.5184  51.1854 13.45031380536428

Epoch: 2026-04-29T22:41Z

TLE epoch observation values (Epoch: 2026-04-29T22:41:48.321Z)

Latitude

-0.00004°

Longitude

160.6008°

Altitude

1,072.059 km

Speed

7.326 km/s

True Right ascension

23h 55m 48s

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

09:33:33

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,122.04 km

Perigee altitude

1,053.842 km

Semi-major axis

7,466.078 km

Eccentricity

0.00457

Inclination

100.41°

RAAN

358.9515°

Arg. of periapsis

308.5184°

True anomaly

51.59465°

Mean anomaly

51.1854°

Eccentric anomaly

51.38988°

Mean motion

3.36437 °/min

Orbital period

107 mins

BSTAR

0.0020758

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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.
9 mins	2026-05-06 03:30:18.087Z	50.051° ENE	2026-05-06 03:34:18.087Z	88.902° E	19.601°	2026-05-06 03:39:18.087Z	138.373° SSE
11 mins	2026-05-06 05:15:18.087Z	7.896° NNE	2026-05-06 05:20:18.087Z	303.441° NW	42.508°	2026-05-06 05:26:18.087Z	210.694° SW
11 mins	2026-05-06 15:29:18.087Z	150.179° SSE	2026-05-06 15:34:18.087Z	72.642° E	43.223°	2026-05-06 15:40:18.087Z	349.877° N
7 mins	2026-05-06 17:17:18.087Z	235.699° WSW	2026-05-06 17:20:18.087Z	267.497° W	18.367°	2026-05-06 17:24:18.087Z	307.153° NW

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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: 6 days ago

TLE from 6 days ago

TLE epoch observation values (Epoch: 2026-04-29T22:41:48.321Z)

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: 6 days ago