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, 0.1 m

Radar Cross Section

Small (<0.1 m²)

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Last TLE update: 12 hours ago

TLE from 12 hours ago

0 NIMBUS 2 DEB
1 24956U 66040C   26087.95488354  .00002319  00000-0  29200-2 0  9991
2 24956 100.4725 272.0371 0044637 231.0385 287.7065 13.64775607928443

Epoch: 2026-03-28T22:55Z

TLE epoch observation values (Epoch: 2026-03-28T22:55:01.937Z)

Latitude

21.37478°

Longitude

-73.9615°

Altitude

1,010.975 km

Speed

7.353 km/s

True Right ascension

06h 24m 39s

True Declination

21° 15' 44"

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

16:27:13

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,048.714 km

Perigee altitude

982.706 km

Semi-major axis

7,393.847 km

Eccentricity

0.00446

Inclination

100.4725°

RAAN

272.0371°

Arg. of periapsis

231.0385°

True anomaly

287.21841°

Mean anomaly

287.7065°

Eccentric anomaly

287.46254°

Mean motion

3.4138 °/min

Orbital period

105.45 mins

BSTAR

0.00292

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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	2026-03-29 12:19:14.463Z	174.368° S	2026-03-29 12:24:14.463Z	230.919° WSW	42.531°	2026-03-29 12:30:14.463Z	337.767° N
11 mins	2026-03-30 01:08:14.463Z	18.768° NNE	2026-03-30 01:13:14.463Z	137.719° SSE	44.601°	2026-03-30 01:19:14.463Z	193.823° SSW
5 mins	2026-03-30 02:54:14.463Z	325.069° NNW	2026-03-30 02:56:14.463Z	302.826° NW	16.701°	2026-03-30 02:59:14.463Z	271.378° WNW

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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, 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: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-03-28T22:55:01.937Z)

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: 12 hours ago