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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https://www.satcat.com/sats-embedded/28203?theme=dark&initialShowStats=false

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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, 0.054 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 28203U 66040R   26304.96362314  .00001019  00000-0  16309-2 0  9992
2 28203 100.3240 199.5459 0052214 312.8353  60.4903 13.51292182203324

Epoch: 2026-10-31T23:07Z

TLE epoch observation values (Epoch: 2026-10-31T23:07:37.039Z)

Latitude

13.58856°

Longitude

169.86915°

Altitude

1,050.538 km

Speed

7.337 km/s

True Right ascension

13h 08m 08s

True Declination

13° 30' 48"

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

00:58:14

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,103.703 km

Perigee altitude

1,025.978 km

Semi-major axis

7,442.978 km

Eccentricity

0.00522

Inclination

100.324°

RAAN

199.5459°

Arg. of periapsis

312.8353°

True anomaly

61.01268°

Mean anomaly

60.4903°

Eccentric anomaly

60.75132°

Mean motion

3.38005 °/min

Orbital period

106.51 mins

BSTAR

0.0016309

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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	2026-11-02 05:51:43.660Z	20.827° NNE	2026-11-02 05:57:43.660Z	105.285° ESE	71.47°	2026-11-02 06:03:43.660Z	187.541° SSW
8 mins	2026-11-02 07:38:43.660Z	336.992° NNW	2026-11-02 07:41:43.660Z	305.109° NW	21.744°	2026-11-02 07:46:43.660Z	255.863° W
10 mins	2026-11-02 16:04:43.660Z	119.685° SE	2026-11-02 16:08:43.660Z	66.799° ENE	36.95°	2026-11-02 16:14:43.660Z	0.624° NNE
10 mins	2026-11-02 17:49:43.660Z	205.247° SW	2026-11-02 17:53:43.660Z	261.467° W	37.95°	2026-11-02 17:59:43.660Z	328.146° NNW
10 mins	2026-11-03 04:59:43.660Z	44.695° NE	2026-11-03 05:04:43.660Z	102.39° ESE	28.251°	2026-11-03 05:09:43.660Z	152.357° SSE

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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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-10-31T23:07:37.039Z)

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: 1 day ago