NIMBUS 2 DEB, 42442

Orbit data source: Space-Track

NIMBUS 2 DEB, 42442 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/42442?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

42442, 1966-040BV

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: 3 days ago

TLE from 3 days ago

0 NIMBUS 2 DEB
1 42442U 66040BV  26260.41102444  .00003820  00000-0  53353-2 0  9992
2 42442 100.3130 115.3412 0048293 301.1424  58.4981 13.57729245245500

Epoch: 2026-09-17T09:51Z

TLE epoch observation values (Epoch: 2026-09-17T09:51:52.511Z)

Latitude

-0.00002°

Longitude

-28.97624°

Altitude

1,028.124 km

Speed

7.347 km/s

True Right ascension

07h 41m 21s

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

19:20:21

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,077.11 km

Perigee altitude

1,005.449 km

Semi-major axis

7,419.417 km

Eccentricity

0.00483

Inclination

100.313°

RAAN

115.3412°

Arg. of periapsis

301.1424°

True anomaly

58.97143°

Mean anomaly

58.4981°

Eccentric anomaly

58.73461°

Mean motion

3.39616 °/min

Orbital period

106 mins

BSTAR

0.0053353

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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 03:52:49.542Z	6.704° NNE	2026-09-20 03:58:49.542Z	289.334° WNW	58.527°	2026-09-20 04:04:49.542Z	214.655° SW
4 mins	2026-09-20 12:21:49.542Z	68.966° E	2026-09-20 12:23:49.542Z	50.092° ENE	12.395°	2026-09-20 12:25:49.542Z	31.747° NE
11 mins	2026-09-20 14:01:49.542Z	151.105° SSE	2026-09-20 14:06:49.542Z	74.683° E	70.362°	2026-09-20 14:12:49.542Z	349.732° N
7 mins	2026-09-20 15:48:49.542Z	235.044° WSW	2026-09-20 15:51:49.542Z	266.889° W	18.536°	2026-09-20 15:55:49.542Z	307.076° 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, 42442 on other resources

View NIMBUS 2 DEB, 42442 on Heavens-Above

View NIMBUS 2 DEB, 42442 on Keep Track

View NIMBUS 2 DEB, 42442 on Celestrak

View NIMBUS 2 DEB, 42442 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, 42442

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: 2026-09-17T09:51:52.511Z)

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, 42442 on other resources

Documentation

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