NIMBUS 2 DEB, 24956

Orbit data source: Space-Track

NIMBUS 2 DEB, 24956 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/24956?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

24956, 1966-040C

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, 0.065 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago

0 NIMBUS 2 DEB
1 24956U 66040C   26313.50237898  .00002371  00000-0  29423-2 0  9994
2 24956 100.4608 155.1218 0045640  27.1839   2.8526 13.65591356959223

Epoch: 2026-11-09T12:03Z

TLE epoch observation values (Epoch: 2026-11-09T12:03:25.543Z)

Latitude

29.56298°

Longitude

-80.39274°

Altitude

985.297 km

Speed

7.378 km/s

True Right ascension

09h 56m 34s

True Declination

29° 25' 13"

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

03:01:12

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,046.495 km

Perigee altitude

979.03 km

Semi-major axis

7,390.9 km

Eccentricity

0.00456

Inclination

100.4608°

RAAN

155.1218°

Arg. of periapsis

27.1839°

True anomaly

2.87878°

Mean anomaly

2.8526°

Eccentric anomaly

2.86567°

Mean motion

3.41584 °/min

Orbital period

105.39 mins

BSTAR

0.0029423

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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	2026-11-10 12:38:53.828Z	131.946° SE	2026-11-10 12:44:53.828Z	54.944° ENE	38.974°	2026-11-10 12:49:53.828Z	359.884° N
8 mins	2026-11-10 14:24:53.828Z	213.238° SW	2026-11-10 14:27:53.828Z	253.985° W	31.459°	2026-11-10 14:32:53.828Z	319.304° NNW
8 mins	2026-11-11 01:27:53.828Z	50.772° ENE	2026-11-11 01:31:53.828Z	99.503° ESE	25.842°	2026-11-11 01:35:53.828Z	144.561° SSE
10 mins	2026-11-11 03:10:53.828Z	1.626° NNE	2026-11-11 03:15:53.828Z	286.918° WNW	51.055°	2026-11-11 03:20:53.828Z	221.385° 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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Check out NIMBUS 2 DEB, 24956 on other resources

View NIMBUS 2 DEB, 24956 on Heavens-Above

View NIMBUS 2 DEB, 24956 on Keep Track

View NIMBUS 2 DEB, 24956 on Celestrak

View NIMBUS 2 DEB, 24956 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, 24956

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 19 hours ago

TLE from 19 hours ago

TLE epoch observation values (Epoch: 2026-11-09T12:03:25.543Z)

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, 24956 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 19 hours ago