NIMBUS 2 DEB, 39294

Orbit data source: Space-Track

NIMBUS 2 DEB, 39294 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/39294?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39294, 1966-040BC

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: 17 hours ago

TLE from 17 hours ago

0 NIMBUS 2 DEB
1 39294U 66040BC  26215.66928604  .00001401  00000-0  23486-2 0  9991
2 39294 100.4419 121.7910 0059454  52.7346 307.9186 13.47356847626087

Epoch: 2026-08-03T16:03Z

TLE epoch observation values (Epoch: 2026-08-03T16:03:46.313Z)

Latitude

-0.00004°

Longitude

-71.40104°

Altitude

1,057.658 km

Speed

7.336 km/s

True Right ascension

08h 07m 09s

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

22:54:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,123.681 km

Perigee altitude

1,035.006 km

Semi-major axis

7,457.48 km

Eccentricity

0.00595

Inclination

100.4419°

RAAN

121.791°

Arg. of periapsis

52.7346°

True anomaly

307.37868°

Mean anomaly

307.9186°

Eccentric anomaly

307.64889°

Mean motion

3.37019 °/min

Orbital period

106.82 mins

BSTAR

0.0023486

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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 17:07:59.119Z	141.298° SSE	2026-08-04 17:12:59.119Z	78.422° E	38.934°	2026-08-04 17:18:59.119Z	354.516° N
8 mins	2026-08-04 18:54:59.119Z	220.996° SW	2026-08-04 18:58:59.119Z	267.12° W	21.96°	2026-08-04 19:02:59.119Z	311.299° NW
11 mins	2026-08-05 06:05:59.119Z	35.05° NE	2026-08-05 06:10:59.119Z	103.806° ESE	34.419°	2026-08-05 06:16:59.119Z	170.274° S
9 mins	2026-08-05 07:51:59.119Z	347.189° N	2026-08-05 07:55:59.119Z	294.971° NW	28.578°	2026-08-05 08:00:59.119Z	239.092° 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, 39294 on other resources

View NIMBUS 2 DEB, 39294 on Heavens-Above

View NIMBUS 2 DEB, 39294 on Keep Track

View NIMBUS 2 DEB, 39294 on Celestrak

View NIMBUS 2 DEB, 39294 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, 39294

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2026-08-03T16:03:46.313Z)

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, 39294 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago