NIMBUS 2 DEB, 28203

Orbit data source: Space-Track

NIMBUS 2 DEB, 28203 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/28203?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28203, 1966-040R

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: 17 hours ago

TLE from 17 hours ago

0 NIMBUS 2 DEB
1 28203U 66040R   26130.22829931  .00001431  00000-0  22724-2 0  9997
2 28203 100.3324  18.1597 0052042  16.0055 110.3513 13.50908605179728

Epoch: 2026-05-10T05:28Z

TLE epoch observation values (Epoch: 2026-05-10T05:28:45.060Z)

Latitude

51.96393°

Longitude

-98.65611°

Altitude

1,090.866 km

Speed

7.305 km/s

True Right ascension

14h 06m 15s

True Declination

51° 48' 16"

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

06:57:52

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,104.993 km

Perigee altitude

1,027.509 km

Semi-major axis

7,444.388 km

Eccentricity

0.0052

Inclination

100.3324°

RAAN

18.1597°

Arg. of periapsis

16.0055°

True anomaly

110.90916°

Mean anomaly

110.3513°

Eccentric anomaly

110.63036°

Mean motion

3.37909 °/min

Orbital period

106.54 mins

BSTAR

0.0022724

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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.
11 mins	2026-05-11 04:34:23.059Z	37.585° NE	2026-05-11 04:39:23.059Z	94.713° ESE	29.601°	2026-05-11 04:45:23.059Z	161.145° S
10 mins	2026-05-11 06:20:23.059Z	352.628° N	2026-05-11 06:24:23.059Z	298.022° NW	33.274°	2026-05-11 06:30:23.059Z	228.288° WSW
6 mins	2026-05-11 14:49:23.059Z	84.371° E	2026-05-11 14:51:23.059Z	62.557° ENE	17.541°	2026-05-11 14:55:23.059Z	20.623° NNE
11 mins	2026-05-11 16:31:23.059Z	170.548° S	2026-05-11 16:36:23.059Z	282.641° WNW	44.055°	2026-05-11 16:42:23.059Z	341.443° N

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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, 28203 on other resources

View NIMBUS 2 DEB, 28203 on Heavens-Above

View NIMBUS 2 DEB, 28203 on Keep Track

View NIMBUS 2 DEB, 28203 on Celestrak

View NIMBUS 2 DEB, 28203 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, 28203

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2026-05-10T05:28:45.060Z)

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, 28203 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago