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

Medium (>0.1 m² and <1 m²)

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

TLE from 2 days ago

0 NIMBUS 2 DEB
1 42435U 66040BN  26214.42406125  .00001241  00000-0  22064-2 0  9997
2 42435 100.2108  20.5876 0052862  66.4465 294.2205 13.43930107481811

Epoch: 2026-08-02T10:10Z

TLE epoch observation values (Epoch: 2026-08-02T10:10:38.892Z)

Latitude

-0.00004°

Longitude

-83.09616°

Altitude

1,081.4 km

Speed

7.319 km/s

True Right ascension

01h 22m 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

19:01:52

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,131.5 km

Perigee altitude

1,052.522 km

Semi-major axis

7,470.148 km

Eccentricity

0.00529

Inclination

100.2108°

RAAN

20.5876°

Arg. of periapsis

66.4465°

True anomaly

293.66658°

Mean anomaly

294.2205°

Eccentric anomaly

293.94369°

Mean motion

3.36163 °/min

Orbital period

107.09 mins

BSTAR

0.0022064

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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.
11 mins	2026-08-04 10:32:11.376Z	144.002° SSE	2026-08-04 10:37:11.376Z	83.636° E	40.038°	2026-08-04 10:43:11.376Z	354.031° N
8 mins	2026-08-04 12:20:11.376Z	228.127° WSW	2026-08-04 12:23:11.376Z	262.153° W	20.983°	2026-08-04 12:28:11.376Z	314.568° NW
11 mins	2026-08-04 23:32:11.376Z	31.744° NE	2026-08-04 23:37:11.376Z	103.214° ESE	37.077°	2026-08-04 23:43:11.376Z	173.953° S
9 mins	2026-08-05 01:18:11.376Z	346.945° N	2026-08-05 01:22:11.376Z	300.207° NW	26.16°	2026-08-05 01:27:11.376Z	244.298° WSW

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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: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-08-02T10:10:38.892Z)

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: 2 days ago