NIMBUS 2 DEB, 39295

Orbit data source: Space-Track

NIMBUS 2 DEB, 39295 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/39295?theme=dark&initialShowStats=false

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Identifier

39295, 1966-040BD

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: 3 days ago

TLE from 3 days ago

0 NIMBUS 2 DEB
1 39295U 66040BD  26131.57192666  .00001394  00000-0  22729-2 0  9990
2 39295 100.4261  66.4662 0060120 271.2613  88.1631 13.49155148615375

Epoch: 2026-05-11T13:43Z

TLE epoch observation values (Epoch: 2026-05-11T13:43:34.463Z)

Latitude

-0.00004°

Longitude

-8.78612°

Altitude

1,076.96 km

Speed

7.314 km/s

True Right ascension

04h 25m 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

16:47:16

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,117.504 km

Perigee altitude

1,027.915 km

Semi-major axis

7,450.847 km

Eccentricity

0.00601

Inclination

100.4261°

RAAN

66.4662°

Arg. of periapsis

271.2613°

True anomaly

88.85182°

Mean anomaly

88.1631°

Eccentric anomaly

88.50745°

Mean motion

3.3747 °/min

Orbital period

106.68 mins

BSTAR

0.0022729

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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	2026-05-14 09:57:22.749Z	344.559° N	2026-05-14 10:01:22.749Z	299.58° NW	24.083°	2026-05-14 10:06:22.749Z	247.927° W
10 mins	2026-05-14 18:24:22.749Z	115.204° SE	2026-05-14 18:29:22.749Z	54.679° ENE	27.551°	2026-05-14 18:34:22.749Z	4.683° NNE
10 mins	2026-05-14 20:09:22.749Z	194.946° SSW	2026-05-14 20:13:22.749Z	249.992° W	36.05°	2026-05-14 20:19:22.749Z	329.707° NNW
9 mins	2026-05-15 07:21:22.749Z	51.325° ENE	2026-05-15 07:25:22.749Z	94.333° ESE	21.502°	2026-05-15 07:30:22.749Z	144.285° SSE

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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, 39295 on other resources

View NIMBUS 2 DEB, 39295 on Heavens-Above

View NIMBUS 2 DEB, 39295 on Keep Track

View NIMBUS 2 DEB, 39295 on Celestrak

View NIMBUS 2 DEB, 39295 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, 39295

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-05-11T13:43:34.463Z)

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, 39295 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago