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)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 NIMBUS 2 DEB
1 28200U 66040N   26035.23643280 -.00001346  00000-0 -29604-2 0  9991
2 28200  99.6387 128.2864 0040576 303.5745  81.4402 13.25887033114034

Epoch: 2026-02-04T05:40Z

TLE epoch observation values (Epoch: 2026-02-04T05:40:27.793Z)

Latitude

25.11901°

Longitude

-95.77899°

Altitude

1,160.787 km

Speed

7.277 km/s

True Right ascension

08h 14m 58s

True Declination

24° 59' 39"

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

11:35:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,190.233 km

Perigee altitude

1,129.062 km

Semi-major axis

7,537.784 km

Eccentricity

0.00406

Inclination

99.6387°

RAAN

128.2864°

Arg. of periapsis

303.5745°

True anomaly

81.90033°

Mean anomaly

81.4402°

Eccentric anomaly

81.67023°

Mean motion

3.31648 °/min

Orbital period

108.55 mins

BSTAR

-0.0029604

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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	2026-02-05 18:22:39.079Z	28.015° NE	2026-02-05 18:28:39.079Z	96.769° ESE	36.965°	2026-02-05 18:34:39.079Z	170.341° S
10 mins	2026-02-05 20:10:39.079Z	350.036° N	2026-02-05 20:15:39.079Z	294.359° NW	28.162°	2026-02-05 20:20:39.079Z	241.852° WSW
9 mins	2026-02-06 04:47:39.079Z	109.544° ESE	2026-02-06 04:51:39.079Z	63.759° ENE	26.619°	2026-02-06 04:56:39.079Z	10.197° NNE
11 mins	2026-02-06 06:33:39.079Z	191.365° SSW	2026-02-06 06:38:39.079Z	266.546° W	38.036°	2026-02-06 06:44:39.079Z	333.713° 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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-02-04T05:40:27.793Z)

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: 1 day ago