NIMBUS 2 DEB, 28620

Orbit data source: Space-Track

NIMBUS 2 DEB, 28620 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/28620?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28620, 1966-040AK

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: 19 hours ago

TLE from 19 hours ago

0 NIMBUS 2 DEB
1 28620U 66040AK  26060.24000185  .00002345  00000-0  36254-2 0  9994
2 28620 100.4402 326.5441 0040590 286.6401 227.1767 13.52025289 36627

Epoch: 2026-03-01T05:45Z

TLE epoch observation values (Epoch: 2026-03-01T05:45:36.159Z)

Latitude

26.0849°

Longitude

-93.75822°

Altitude

1,088.453 km

Speed

7.3 km/s

True Right ascension

10h 06m 46s

True Declination

25° 57' 19"

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

04:42:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,092.355 km

Perigee altitude

1,031.954 km

Semi-major axis

7,440.291 km

Eccentricity

0.00406

Inclination

100.4402°

RAAN

326.5441°

Arg. of periapsis

286.6401°

True anomaly

226.83673°

Mean anomaly

227.1767°

Eccentric anomaly

227.0066°

Mean motion

3.38188 °/min

Orbital period

106.45 mins

BSTAR

0.0036254

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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	2026-03-02 06:27:11.793Z	19.815° NNE	2026-03-02 06:33:11.793Z	87.604° E	43.77°	2026-03-02 06:39:11.793Z	188.977° SSW
7 mins	2026-03-02 08:14:11.793Z	338.212° N	2026-03-02 08:17:11.793Z	307.234° NW	19.344°	2026-03-02 08:21:11.793Z	264.834° W
10 mins	2026-03-02 16:40:11.793Z	121.017° SE	2026-03-02 16:44:11.793Z	65.824° ENE	32.191°	2026-03-02 16:50:11.793Z	359.513° N
9 mins	2026-03-02 18:25:11.793Z	207.886° SW	2026-03-02 18:29:11.793Z	263.658° W	30.545°	2026-03-02 18:34:11.793Z	322.891° 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, 28620 on other resources

View NIMBUS 2 DEB, 28620 on Heavens-Above

View NIMBUS 2 DEB, 28620 on Keep Track

View NIMBUS 2 DEB, 28620 on Celestrak

View NIMBUS 2 DEB, 28620 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, 28620

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 19 hours ago

TLE from 19 hours ago

TLE epoch observation values (Epoch: 2026-03-01T05:45:36.159Z)

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, 28620 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 19 hours ago