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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago

0 NIMBUS 2 DEB
1 25825U 66040H   26258.74064128  .00002019  00000-0  23203-2 0  9997
2 25825 100.3312 345.4786 0043625 299.8375 213.9532 13.70510569949682

Epoch: 2026-09-15T17:46Z

TLE epoch observation values (Epoch: 2026-09-15T17:46:31.406Z)

Latitude

26.05955°

Longitude

-90.76655°

Altitude

1,027.53 km

Speed

7.327 km/s

True Right ascension

11h 22m 15s

True Declination

25° 55' 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

07:40:04

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,027.212 km

Perigee altitude

962.881 km

Semi-major axis

7,373.183 km

Eccentricity

0.00436

Inclination

100.3312°

RAAN

345.4786°

Arg. of periapsis

299.8375°

True anomaly

213.67525°

Mean anomaly

213.9532°

Eccentric anomaly

213.8141°

Mean motion

3.42816 °/min

Orbital period

105.01 mins

BSTAR

0.0023203

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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	2026-09-16 18:09:15.289Z	32.233° NE	2026-09-16 18:14:15.289Z	89.906° E	41.059°	2026-09-16 18:20:15.289Z	167.781° S
9 mins	2026-09-16 19:54:15.289Z	346.691° N	2026-09-16 19:58:15.289Z	291.702° WNW	33.001°	2026-09-16 20:03:15.289Z	236.664° WSW
6 mins	2026-09-17 04:15:15.289Z	87.92° E	2026-09-17 04:18:15.289Z	53.831° ENE	19.035°	2026-09-17 04:21:15.289Z	22.181° NNE
10 mins	2026-09-17 05:56:15.289Z	172.309° S	2026-09-17 06:01:15.289Z	293.77° NW	70.417°	2026-09-17 06:06:15.289Z	339.936° 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: 21 hours ago

TLE from 21 hours ago

TLE epoch observation values (Epoch: 2026-09-15T17:46:31.406Z)

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: 21 hours ago