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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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: 13 hours ago

TLE from 13 hours ago

0 NIMBUS 2 DEB
1 28200U 66040N   26087.71011927 -.00001056  00000-0 -22953-2 0  9996
2 28200  99.6370 176.9489 0060448 187.6845 326.3088 13.25763718120986

Epoch: 2026-03-28T17:02Z

TLE epoch observation values (Epoch: 2026-03-28T17:02:34.304Z)

Latitude

26.02626°

Longitude

-80.08876°

Altitude

1,127.96 km

Speed

7.309 km/s

True Right ascension

00h 06m 43s

True Declination

25° 53' 51"

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

11:30:14

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,205.682 km

Perigee altitude

1,114.548 km

Semi-major axis

7,538.252 km

Eccentricity

0.00604

Inclination

99.637°

RAAN

176.9489°

Arg. of periapsis

187.6845°

True anomaly

325.92213°

Mean anomaly

326.3088°

Eccentric anomaly

326.11571°

Mean motion

3.31617 °/min

Orbital period

108.56 mins

BSTAR

-0.0022953

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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	2026-03-29 06:51:04.013Z	204.638° SW	2026-03-29 06:57:04.013Z	263.841° W	27.741°	2026-03-29 07:03:04.013Z	324.102° NNW
11 mins	2026-03-29 18:15:04.013Z	30.23° NE	2026-03-29 18:20:04.013Z	97.107° ESE	37.631°	2026-03-29 18:26:04.013Z	172.847° S
9 mins	2026-03-29 20:03:04.013Z	342.932° N	2026-03-29 20:07:04.013Z	294.709° NW	26.159°	2026-03-29 20:12:04.013Z	243.142° WSW
10 mins	2026-03-30 04:39:04.013Z	112.505° SE	2026-03-30 04:43:04.013Z	67.07° ENE	28.135°	2026-03-30 04:49:04.013Z	5.365° NNE

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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: 13 hours ago

TLE from 13 hours ago

TLE epoch observation values (Epoch: 2026-03-28T17:02:34.304Z)

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: 13 hours ago