NIMBUS 2 DEB, 25526

Orbit data source: Space-Track

NIMBUS 2 DEB, 25526 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/25526?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

25526, 1966-040D

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: 22 hours ago

TLE from 22 hours ago

0 NIMBUS 2 DEB
1 25526U 66040D   26215.32084902  .00002276  00000-0  22055-2 0  9993
2 25526 100.5820 335.8034 0035739  15.8601   8.7761 13.80702425672110

Epoch: 2026-08-03T07:42Z

TLE epoch observation values (Epoch: 2026-08-03T07:42:01.355Z)

Latitude

24.27824°

Longitude

-96.41644°

Altitude

938.296 km

Speed

7.398 km/s

True Right ascension

22h 03m 58s

True Declination

24° 09' 10"

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

19:03:02

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

984.926 km

Perigee altitude

932.484 km

Semi-major axis

7,336.842 km

Eccentricity

0.00357

Inclination

100.582°

RAAN

335.8034°

Arg. of periapsis

15.8601°

True anomaly

8.83886°

Mean anomaly

8.7761°

Eccentric anomaly

8.80745°

Mean motion

3.45366 °/min

Orbital period

104.24 mins

BSTAR

0.0022055

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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.
6 mins	2026-08-04 06:22:21.046Z	89.684° E	2026-08-04 06:25:21.046Z	57.267° ENE	15.69°	2026-08-04 06:28:21.046Z	24.718° NE
9 mins	2026-08-04 08:03:21.046Z	168.497° S	2026-08-04 08:07:21.046Z	245.856° WSW	44.582°	2026-08-04 08:12:21.046Z	341.076° N
10 mins	2026-08-04 20:42:21.046Z	29.077° NE	2026-08-04 20:46:21.046Z	84.125° E	39.381°	2026-08-04 20:52:21.046Z	179.885° S
7 mins	2026-08-04 22:26:21.046Z	335.105° NNW	2026-08-04 22:29:21.046Z	296.224° NW	21.859°	2026-08-04 22:33:21.046Z	252.014° W

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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, 25526 on other resources

View NIMBUS 2 DEB, 25526 on Heavens-Above

View NIMBUS 2 DEB, 25526 on Keep Track

View NIMBUS 2 DEB, 25526 on Celestrak

View NIMBUS 2 DEB, 25526 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, 25526

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 22 hours ago

TLE from 22 hours ago

TLE epoch observation values (Epoch: 2026-08-03T07:42:01.355Z)

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, 25526 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 22 hours ago