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: 6 days ago

TLE from 6 days ago

0 NIMBUS 2 DEB
1 42436U 66040BP  26081.82221629  .00001998  00000-0  33981-2 0  9997
2 42436 100.3144 289.1191 0048642  24.7686 335.5764 13.45999260528312

Epoch: 2026-03-22T19:43Z

TLE epoch observation values (Epoch: 2026-03-22T19:43:59.487Z)

Latitude

-0.00007°

Longitude

172.79819°

Altitude

1,056.735 km

Speed

7.34 km/s

True Right ascension

19h 16m 28s

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

10:01:00

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,120.653 km

Perigee altitude

1,048.055 km

Semi-major axis

7,462.491 km

Eccentricity

0.00486

Inclination

100.3144°

RAAN

289.1191°

Arg. of periapsis

24.7686°

True anomaly

335.34465°

Mean anomaly

335.5764°

Eccentric anomaly

335.46065°

Mean motion

3.3668 °/min

Orbital period

106.93 mins

BSTAR

0.0033981

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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.
9 mins	2026-03-29 12:26:04.518Z	113.013° SE	2026-03-29 12:31:04.518Z	55.397° ENE	24.853°	2026-03-29 12:35:04.518Z	11.567° NNE
10 mins	2026-03-29 14:11:04.518Z	189.404° SSW	2026-03-29 14:16:04.518Z	269.989° W	37.496°	2026-03-29 14:21:04.518Z	331.088° NNW
8 mins	2026-03-30 01:25:04.518Z	56.471° ENE	2026-03-30 01:28:04.518Z	88.343° E	20.444°	2026-03-30 01:33:04.518Z	139.414° SSE
11 mins	2026-03-30 03:09:04.518Z	6.504° NNE	2026-03-30 03:14:04.518Z	299.791° NW	41.751°	2026-03-30 03:20:04.518Z	212.517° SW

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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: 6 days ago

TLE from 6 days ago

TLE epoch observation values (Epoch: 2026-03-22T19:43:59.487Z)

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: 6 days ago