NIMBUS 2 DEB, 42435

Orbit data source: Space-Track

NIMBUS 2 DEB, 42435 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/42435?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

42435, 1966-040BN

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: 17 hours ago

TLE from 17 hours ago

0 NIMBUS 2 DEB
1 42435U 66040BN  26032.88641902  .00001611  00000-0  28676-2 0  9995
2 42435 100.1902 196.8648 0053148 147.8615 212.5772 13.43308509457433

Epoch: 2026-02-01T21:16Z

TLE epoch observation values (Epoch: 2026-02-01T21:16:26.603Z)

Latitude

0.00001°

Longitude

105.66433°

Altitude

1,133.284 km

Speed

7.27 km/s

True Right ascension

13h 07m 27s

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

16:05:10

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,134.031 km

Perigee altitude

1,054.601 km

Semi-major axis

7,472.453 km

Eccentricity

0.00531

Inclination

100.1902°

RAAN

196.8648°

Arg. of periapsis

147.8615°

True anomaly

212.2511°

Mean anomaly

212.5772°

Eccentric anomaly

212.41397°

Mean motion

3.36007 °/min

Orbital period

107.14 mins

BSTAR

0.0028676

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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.
11 mins	2026-02-02 22:54:30.566Z	34.765° NE	2026-02-02 22:59:30.566Z	88.475° E	29.749°	2026-02-02 23:05:30.566Z	161.137° S
9 mins	2026-02-03 00:41:30.566Z	351.093° N	2026-02-03 00:45:30.566Z	296.375° NW	31.773°	2026-02-03 00:50:30.566Z	233.562° WSW
7 mins	2026-02-03 09:12:30.566Z	93.189° ESE	2026-02-03 09:15:30.566Z	60.996° ENE	20.088°	2026-02-03 09:19:30.566Z	19.005° NNE
11 mins	2026-02-03 10:55:30.566Z	174.384° S	2026-02-03 11:00:30.566Z	246.311° WSW	43.346°	2026-02-03 11:06:30.566Z	339.031° 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, 42435 on other resources

View NIMBUS 2 DEB, 42435 on Heavens-Above

View NIMBUS 2 DEB, 42435 on Keep Track

View NIMBUS 2 DEB, 42435 on Celestrak

View NIMBUS 2 DEB, 42435 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, 42435

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2026-02-01T21:16:26.603Z)

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, 42435 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago