NIMBUS 2 DEB, 28200

Orbit data source: Space-Track

NIMBUS 2 DEB, 28200 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/28200?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28200, 1966-040N

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: 12 hours ago

TLE from 12 hours ago

0 NIMBUS 2 DEB
1 28200U 66040N   25336.25367566 -.00003254  00000-0 -72452-2 0  9995
2 28200  99.6422  68.9192 0047776 122.0162 265.2497 13.26165583105557

Epoch: 2025-12-02T06:05Z

TLE epoch observation values (Epoch: 2025-12-02T06:05:17.577Z)

Latitude

26.34836°

Longitude

-98.54784°

Altitude

1,167.484 km

Speed

7.27 km/s

True Right ascension

04h 16m 28s

True Declination

26° 13' 09"

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

15:48:25

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,194.599 km

Perigee altitude

1,122.584 km

Semi-major axis

7,536.728 km

Eccentricity

0.00478

Inclination

99.6422°

RAAN

68.9192°

Arg. of periapsis

122.0162°

True anomaly

264.70439°

Mean anomaly

265.2497°

Eccentric anomaly

264.97701°

Mean motion

3.31718 °/min

Orbital period

108.53 mins

BSTAR

-0.0072452

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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	2025-12-02 19:13:34.524Z	15.946° NNE	2025-12-02 19:19:34.524Z	98.024° ESE	44.907°	2025-12-02 19:25:34.524Z	194.15° SSW
6 mins	2025-12-02 21:03:34.524Z	325.621° NNW	2025-12-02 21:05:34.524Z	305.135° NW	16.844°	2025-12-02 21:09:34.524Z	267.164° W
11 mins	2025-12-03 05:37:34.524Z	136.55° SSE	2025-12-03 05:42:34.524Z	64.306° ENE	38.217°	2025-12-03 05:48:34.524Z	356.377° N
9 mins	2025-12-03 07:25:34.524Z	218.978° SW	2025-12-03 07:29:34.524Z	263.961° W	25.091°	2025-12-03 07:34:34.524Z	317.329° 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, 28200 on other resources

View NIMBUS 2 DEB, 28200 on Heavens-Above

View NIMBUS 2 DEB, 28200 on Keep Track

View NIMBUS 2 DEB, 28200 on Celestrak

View NIMBUS 2 DEB, 28200 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, 28200

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2025-12-02T06:05:17.577Z)

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, 28200 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago