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)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago

0 NIMBUS 2 DEB
1 24956U 66040C   26032.08041610  .00002003  00000-0  25438-2 0  9994
2 24956 100.4665 211.8649 0040881   8.1788 112.1749 13.64523324920823

Epoch: 2026-02-01T01:55Z

TLE epoch observation values (Epoch: 2026-02-01T01:55:47.951Z)

Latitude

57.74639°

Longitude

-111.44814°

Altitude

1,040.426 km

Speed

7.331 km/s

True Right ascension

03h 15m 11s

True Declination

57° 35' 49"

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

22:10:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,046.852 km

Perigee altitude

986.391 km

Semi-major axis

7,394.759 km

Eccentricity

0.00409

Inclination

100.4665°

RAAN

211.8649°

Arg. of periapsis

8.1788°

True anomaly

112.60787°

Mean anomaly

112.1749°

Eccentric anomaly

112.39147°

Mean motion

3.41316 °/min

Orbital period

105.47 mins

BSTAR

0.0025438

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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	2026-02-02 00:48:39.460Z	17.78° NNE	2026-02-02 00:53:39.460Z	60.062° ENE	44.655°	2026-02-02 00:59:39.460Z	194.428° SSW
6 mins	2026-02-02 02:34:39.460Z	329.377° NNW	2026-02-02 02:36:39.460Z	308.23° NW	16.509°	2026-02-02 02:40:39.460Z	267.627° W
9 mins	2026-02-02 10:55:39.460Z	121.567° SE	2026-02-02 10:59:39.460Z	60.048° ENE	31.957°	2026-02-02 11:04:39.460Z	1.213° NNE
9 mins	2026-02-02 12:39:39.460Z	209.97° SW	2026-02-02 12:43:39.460Z	267.181° W	28.412°	2026-02-02 12:48:39.460Z	323.742° 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, 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: 18 hours ago

TLE from 18 hours ago

TLE epoch observation values (Epoch: 2026-02-01T01:55:47.951Z)

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: 18 hours ago