NIMBUS 2 DEB, 25825

Orbit data source: Space-Track

NIMBUS 2 DEB, 25825 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/25825?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

25825, 1966-040H

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: 8 hours ago

TLE from 8 hours ago

0 NIMBUS 2 DEB
1 25825U 66040H   26128.16801455  .00002487  00000-0  28702-2 0  9999
2 25825 100.3254 205.4112 0044105 265.4118 150.7515 13.69958901931801

Epoch: 2026-05-08T04:01Z

TLE epoch observation values (Epoch: 2026-05-08T04:01:56.457Z)

Latitude

55.13533°

Longitude

-96.15707°

Altitude

1,037.176 km

Speed

7.324 km/s

True Right ascension

12h 41m 19s

True Declination

54° 58' 48"

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

20:17:47

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,029.555 km

Perigee altitude

964.499 km

Semi-major axis

7,375.164 km

Eccentricity

0.00441

Inclination

100.3254°

RAAN

205.4112°

Arg. of periapsis

265.4118°

True anomaly

150.99726°

Mean anomaly

150.7515°

Eccentric anomaly

150.8745°

Mean motion

3.42678 °/min

Orbital period

105.06 mins

BSTAR

0.0028702

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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.
7 mins	2026-05-08 16:39:53.980Z	56.674° ENE	2026-05-08 16:42:53.980Z	87.172° E	16.707°	2026-05-08 16:46:53.980Z	129.174° SE
10 mins	2026-05-08 18:22:53.980Z	8.771° NNE	2026-05-08 18:27:53.980Z	257.312° W	42.927°	2026-05-08 18:32:53.980Z	207.219° SW
10 mins	2026-05-09 04:25:53.980Z	135.921° SSE	2026-05-09 04:29:53.980Z	79.819° E	37.688°	2026-05-09 04:35:53.980Z	355.843° N
8 mins	2026-05-09 06:10:53.980Z	224.557° SW	2026-05-09 06:13:53.980Z	262.225° W	23.347°	2026-05-09 06:18:53.980Z	317.249° 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, 25825 on other resources

View NIMBUS 2 DEB, 25825 on Heavens-Above

View NIMBUS 2 DEB, 25825 on Keep Track

View NIMBUS 2 DEB, 25825 on Celestrak

View NIMBUS 2 DEB, 25825 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, 25825

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-05-08T04:01:56.457Z)

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, 25825 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago