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)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 NIMBUS 2 DEB
1 25825U 66040H   25336.09873782  .00003543  00000-0  41285-2 0  9998
2 25825 100.3256  37.1985 0046612 301.2936 125.4696 13.68962556910304

Epoch: 2025-12-02T02:22Z

TLE epoch observation values (Epoch: 2025-12-02T02:22:10.947Z)

Latitude

65.16956°

Longitude

-92.5974°

Altitude

1,034.521 km

Speed

7.331 km/s

True Right ascension

00h 56m 32s

True Declination

65° 02' 35"

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

13:48:08

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,035.001 km

Perigee altitude

966.214 km

Semi-major axis

7,378.744 km

Eccentricity

0.00466

Inclination

100.3256°

RAAN

37.1985°

Arg. of periapsis

301.2936°

True anomaly

125.90314°

Mean anomaly

125.4696°

Eccentric anomaly

125.68652°

Mean motion

3.42428 °/min

Orbital period

105.13 mins

BSTAR

0.0041285

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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	2025-12-02 16:40:36.442Z	29.413° NE	2025-12-02 16:45:36.442Z	94.092° ESE	37.442°	2025-12-02 16:51:36.442Z	174.919° S
8 mins	2025-12-02 18:25:36.442Z	342.405° N	2025-12-02 18:29:36.442Z	290.6° WNW	24.986°	2025-12-02 18:33:36.442Z	246.804° WSW
7 mins	2025-12-03 02:46:36.442Z	95.975° ESE	2025-12-03 02:49:36.442Z	59.712° ENE	21.323°	2025-12-03 02:53:36.442Z	15.578° NNE
10 mins	2025-12-03 04:28:36.442Z	182.85° SSW	2025-12-03 04:32:36.442Z	251.784° W	41.088°	2025-12-03 04:38:36.442Z	336.578° 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: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2025-12-02T02:22:10.947Z)

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: 14 hours ago