NIMBUS 2 DEB, 42436

Orbit data source: Space-Track

NIMBUS 2 DEB, 42436 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/42436?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

42436, 1966-040BP

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: 2 days ago

TLE from 2 days ago

0 NIMBUS 2 DEB
1 42436U 66040BP  26149.01081872  .00002060  00000-0  34933-2 0  9996
2 42436 100.3054 358.1307 0043833 223.2169 136.5518 13.46257981537355

Epoch: 2026-05-29T00:15Z

TLE epoch observation values (Epoch: 2026-05-29T00:15:34.737Z)

Latitude

-0.00005°

Longitude

107.68864°

Altitude

1,112.642 km

Speed

7.285 km/s

True Right ascension

23h 52m 31s

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

08:35:49

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,116.102 km

Perigee altitude

1,050.69 km

Semi-major axis

7,461.533 km

Eccentricity

0.00438

Inclination

100.3054°

RAAN

358.1307°

Arg. of periapsis

223.2169°

True anomaly

136.89585°

Mean anomaly

136.5518°

Eccentric anomaly

136.72396°

Mean motion

3.36745 °/min

Orbital period

106.91 mins

BSTAR

0.0034933

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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	2026-05-31 02:48:25.863Z	19.05° NNE	2026-05-31 02:53:25.863Z	67.514° E	44.215°	2026-05-31 02:59:25.863Z	191.66° SSW
7 mins	2026-05-31 04:35:25.863Z	333.824° NNW	2026-05-31 04:38:25.863Z	302.303° NW	17.956°	2026-05-31 04:42:25.863Z	263.26° W
11 mins	2026-05-31 13:02:25.863Z	129.054° SE	2026-05-31 13:07:25.863Z	60.64° ENE	34.712°	2026-05-31 13:13:25.863Z	357.533° N
10 mins	2026-05-31 14:48:25.863Z	210.648° SW	2026-05-31 14:52:25.863Z	259.934° W	28.644°	2026-05-31 14:58:25.863Z	324.583° NNW

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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, 42436 on other resources

View NIMBUS 2 DEB, 42436 on Heavens-Above

View NIMBUS 2 DEB, 42436 on Keep Track

View NIMBUS 2 DEB, 42436 on Celestrak

View NIMBUS 2 DEB, 42436 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, 42436

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-05-29T00:15:34.737Z)

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, 42436 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago