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, 0.071 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 NIMBUS 2 DEB
1 25825U 66040H   26305.21476388  .00002268  00000-0  25826-2 0  9996
2 25825 100.3308  35.3651 0052039 187.6325 201.8118 13.70716690956059

Epoch: 2026-11-01T05:09Z

TLE epoch observation values (Epoch: 2026-11-01T05:09:15.599Z)

Latitude

28.75169°

Longitude

-88.16944°

Altitude

1,036.11 km

Speed

7.319 km/s

True Right ascension

01h 58m 37s

True Declination

28° 36' 44"

Sunlit

Object was in full shadow 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

05:12:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,032.672 km

Perigee altitude

955.941 km

Semi-major axis

7,372.444 km

Eccentricity

0.0052

Inclination

100.3308°

RAAN

35.3651°

Arg. of periapsis

187.6325°

True anomaly

201.59156°

Mean anomaly

201.8118°

Eccentric anomaly

201.70155°

Mean motion

3.42867 °/min

Orbital period

105 mins

BSTAR

0.0025826

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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.
10 mins	2026-11-02 18:24:11.072Z	33.734° NE	2026-11-02 18:29:11.072Z	96.264° ESE	38.556°	2026-11-02 18:34:11.072Z	163.644° S
8 mins	2026-11-02 20:09:11.072Z	345.714° N	2026-11-02 20:12:11.072Z	305.682° NW	32.212°	2026-11-02 20:17:11.072Z	239.231° WSW
6 mins	2026-11-03 04:30:11.072Z	85.789° E	2026-11-03 04:33:11.072Z	51.98° ENE	18.685°	2026-11-03 04:36:11.072Z	21.292° NNE
11 mins	2026-11-03 06:10:11.072Z	169.735° S	2026-11-03 06:15:11.072Z	224.469° SW	75.006°	2026-11-03 06:21:11.072Z	340.818° N

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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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-11-01T05:09:15.599Z)

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: 1 day ago