NIMBUS 2 DEB, 28208

Orbit data source: Space-Track

NIMBUS 2 DEB, 28208 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/28208?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28208, 1966-040W

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)

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Last TLE update: 1 week ago

TLE from 1 week ago

0 NIMBUS 2 DEB
1 28208U 66040W   26150.58711917  .00002484  00000-0  30559-2 0  9991
2 28208 100.3067 185.7521 0039448 283.1036 229.0962 13.66157043252677

Epoch: 2026-05-30T14:05Z

TLE epoch observation values (Epoch: 2026-05-30T14:05:27.096Z)

Latitude

27.68885°

Longitude

-88.26412°

Altitude

1,035.841 km

Speed

7.327 km/s

True Right ascension

00h 44m 47s

True Declination

27° 33' 10"

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

06:09:53

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,039.86 km

Perigee altitude

981.565 km

Semi-major axis

7,388.849 km

Eccentricity

0.00394

Inclination

100.3067°

RAAN

185.7521°

Arg. of periapsis

283.1036°

True anomaly

228.75564°

Mean anomaly

229.0962°

Eccentric anomaly

228.92581°

Mean motion

3.41726 °/min

Orbital period

105.35 mins

BSTAR

0.0030559

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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.
9 mins	2026-06-10 00:50:34.485Z	104.593° ESE	2026-06-10 00:54:34.485Z	63.899° ENE	20.417°	2026-06-10 00:59:34.485Z	12.116° NNE
10 mins	2026-06-10 02:33:34.485Z	177.934° S	2026-06-10 02:38:34.485Z	276.801° WNW	42.069°	2026-06-10 02:43:34.485Z	336.85° NNW
11 mins	2026-06-10 15:20:34.485Z	17.166° NNE	2026-06-10 15:25:34.485Z	58.75° ENE	44.776°	2026-06-10 15:31:34.485Z	194.944° SSW
5 mins	2026-06-10 17:06:34.485Z	327.54° NNW	2026-06-10 17:08:34.485Z	306.248° NW	16.17°	2026-06-10 17:11:34.485Z	274.668° WNW

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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, 28208 on other resources

View NIMBUS 2 DEB, 28208 on Heavens-Above

View NIMBUS 2 DEB, 28208 on Keep Track

View NIMBUS 2 DEB, 28208 on Celestrak

View NIMBUS 2 DEB, 28208 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, 28208

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 week ago

TLE from 1 week ago

TLE epoch observation values (Epoch: 2026-05-30T14:05:27.096Z)

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, 28208 on other resources

Documentation

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