NIMBUS 2 DEB, 28619

Orbit data source: Space-Track

NIMBUS 2 DEB, 28619 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/28619?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28619, 1966-040AJ

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, 0.050 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 28619U 66040AJ  26304.80831109  .00003499  00000-0  28117-2 0  9993
2 28619 100.3055 141.9267 0033291 267.4892 105.8057 13.91105628603830

Epoch: 2026-10-31T19:23Z

TLE epoch observation values (Epoch: 2026-10-31T19:23:58.078Z)

Latitude

13.40445°

Longitude

168.3554°

Altitude

933.533 km

Speed

7.383 km/s

True Right ascension

09h 17m 49s

True Declination

13° 19' 44"

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

22:39:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

946.341 km

Perigee altitude

897.735 km

Semi-major axis

7,300.175 km

Eccentricity

0.00333

Inclination

100.3055°

RAAN

141.9267°

Arg. of periapsis

267.4892°

True anomaly

106.17234°

Mean anomaly

105.8057°

Eccentric anomaly

105.98906°

Mean motion

3.47971 °/min

Orbital period

103.46 mins

BSTAR

0.0028117

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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.
10 mins	2026-11-02 02:59:09.501Z	358.377° N	2026-11-02 03:04:09.501Z	283.484° WNW	42.392°	2026-11-02 03:09:09.501Z	224.614° SW
10 mins	2026-11-02 12:53:09.501Z	149.846° SSE	2026-11-02 12:58:09.501Z	40.922° NE	64.714°	2026-11-02 13:03:09.501Z	350.415° N
5 mins	2026-11-02 14:38:09.501Z	243.594° WSW	2026-11-02 14:40:09.501Z	267.197° W	17.336°	2026-11-02 14:43:09.501Z	300.521° NW
8 mins	2026-11-03 01:28:09.501Z	47.011° ENE	2026-11-03 01:31:09.501Z	90.005° ESE	33.264°	2026-11-03 01:36:09.501Z	158.221° S

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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, 28619 on other resources

View NIMBUS 2 DEB, 28619 on Heavens-Above

View NIMBUS 2 DEB, 28619 on Keep Track

View NIMBUS 2 DEB, 28619 on Celestrak

View NIMBUS 2 DEB, 28619 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, 28619

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: 2026-10-31T19:23:58.078Z)

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, 28619 on other resources

Documentation

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