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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ISO8601 Format

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)

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Last TLE update: 20 hours ago

TLE from 20 hours ago

0 NIMBUS 2 DEB
1 39295U 66040BD  26215.28698462  .00001602  00000-0  25807-2 0  9998
2 39295 100.4218 153.8936 0067387  63.5184 297.2839 13.49438180626666

Epoch: 2026-08-03T06:53Z

TLE epoch observation values (Epoch: 2026-08-03T06:53:15.471Z)

Latitude

0.00001°

Longitude

98.70687°

Altitude

1,054.329 km

Speed

7.336 km/s

True Right ascension

10h 15m 34s

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

16:51:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,121.869 km

Perigee altitude

1,021.465 km

Semi-major axis

7,449.804 km

Eccentricity

0.00674

Inclination

100.4218°

RAAN

153.8936°

Arg. of periapsis

63.5184°

True anomaly

296.59497°

Mean anomaly

297.2839°

Eccentric anomaly

296.9397°

Mean motion

3.37541 °/min

Orbital period

106.65 mins

BSTAR

0.0025807

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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.
12 mins	2026-08-04 08:23:12.340Z	27.031° NE	2026-08-04 08:29:12.340Z	99.117° ESE	37.46°	2026-08-04 08:35:12.340Z	174.843° S
9 mins	2026-08-04 10:10:12.340Z	344.949° N	2026-08-04 10:14:12.340Z	295.812° NW	25.428°	2026-08-04 10:19:12.340Z	243.298° WSW
8 mins	2026-08-04 18:38:12.340Z	107.31° ESE	2026-08-04 18:42:12.340Z	58.175° ENE	24.265°	2026-08-04 18:46:12.340Z	12.541° NNE
10 mins	2026-08-04 20:22:12.340Z	188.986° SSW	2026-08-04 20:27:12.340Z	272.424° WNW	37.353°	2026-08-04 20:32:12.340Z	331.664° 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, 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: 20 hours ago

TLE from 20 hours ago

TLE epoch observation values (Epoch: 2026-08-03T06:53:15.471Z)

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: 20 hours ago