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: 4 days ago

TLE from 4 days ago

0 NIMBUS 2 DEB
1 42442U 66040BV  25332.80514337  .00005751  00000-0  83703-2 0  9999
2 42442 100.3249 168.9652 0051141 295.0370  64.5460 13.54825759205834

Epoch: 2025-11-28T19:19Z

TLE epoch observation values (Epoch: 2025-11-28T19:19:24.387Z)

Latitude

-0.00004°

Longitude

171.17116°

Altitude

1,041.146 km

Speed

7.339 km/s

True Right ascension

11h 15m 51s

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

13:14:55

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,089.882 km

Perigee altitude

1,013.886 km

Semi-major axis

7,430.021 km

Eccentricity

0.00511

Inclination

100.3249°

RAAN

168.9652°

Arg. of periapsis

295.037°

True anomaly

65.0766°

Mean anomaly

64.546°

Eccentric anomaly

64.81115°

Mean motion

3.38889 °/min

Orbital period

106.23 mins

BSTAR

0.0083703

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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	2025-12-03 00:58:28.986Z	47.883° ENE	2025-12-03 01:02:28.986Z	89.368° E	21.874°	2025-12-03 01:07:28.986Z	142.777° SSE
11 mins	2025-12-03 02:42:28.986Z	5.255° NNE	2025-12-03 02:47:28.986Z	306.092° NW	40.05°	2025-12-03 02:53:28.986Z	216.032° SW
11 mins	2025-12-03 12:52:28.986Z	152.135° SSE	2025-12-03 12:57:28.986Z	54.28° ENE	43.619°	2025-12-03 13:03:28.986Z	348.755° N
7 mins	2025-12-03 14:39:28.986Z	236.336° WSW	2025-12-03 14:42:28.986Z	267.539° W	17.161°	2025-12-03 14:46:28.986Z	306.815° 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: 4 days ago

TLE from 4 days ago

TLE epoch observation values (Epoch: 2025-11-28T19:19:24.387Z)

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: 4 days ago