NIMBUS 2 DEB, 28201

Orbit data source: Space-Track

NIMBUS 2 DEB, 28201 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/28201?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28201, 1966-040P

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, 0.058 m

Radar Cross Section

Small (<0.1 m²)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 NIMBUS 2 DEB
1 28201U 66040P   26309.77947659  .00001990  00000-0  25738-2 0  9999
2 28201 100.2593 241.0517 0066234 342.3264  45.3342 13.62807308670507

Epoch: 2026-11-05T18:42Z

TLE epoch observation values (Epoch: 2026-11-05T18:42:26.777Z)

Latitude

27.75557°

Longitude

-90.00563°

Altitude

994.483 km

Speed

7.374 km/s

True Right ascension

15h 42m 27s

True Declination

27° 37' 07"

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

17:49:29

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,071.841 km

Perigee altitude

973.802 km

Semi-major axis

7,400.958 km

Eccentricity

0.00662

Inclination

100.2593°

RAAN

241.0517°

Arg. of periapsis

342.3264°

True anomaly

45.87716°

Mean anomaly

45.3342°

Eccentric anomaly

45.60536°

Mean motion

3.40888 °/min

Orbital period

105.61 mins

BSTAR

0.0025738

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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.
12 mins	2026-11-07 08:09:28.692Z	23.435° NE	2026-11-07 08:15:28.692Z	97.477° ESE	60.631°	2026-11-07 08:21:28.692Z	181.287° SSW
8 mins	2026-11-07 09:55:28.692Z	341.761° N	2026-11-07 09:59:28.692Z	295.818° NW	24.557°	2026-11-07 10:03:28.692Z	253.603° W
8 mins	2026-11-07 18:18:28.692Z	106.014° ESE	2026-11-07 18:21:28.692Z	68.514° E	27.561°	2026-11-07 18:26:28.692Z	9.743° NNE
10 mins	2026-11-07 20:01:28.692Z	192.431° SSW	2026-11-07 20:05:28.692Z	253.188° W	48.114°	2026-11-07 20:11:28.692Z	332.417° 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, 28201 on other resources

View NIMBUS 2 DEB, 28201 on Heavens-Above

View NIMBUS 2 DEB, 28201 on Keep Track

View NIMBUS 2 DEB, 28201 on Celestrak

View NIMBUS 2 DEB, 28201 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, 28201

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: 2026-11-05T18:42:26.777Z)

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, 28201 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago