NIMBUS 2 DEB, 28617

Orbit data source: Space-Track

NIMBUS 2 DEB, 28617 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/28617?theme=dark&initialShowStats=false

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Identifier

28617, 1966-040AG

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: 3 days ago

TLE from 3 days ago

0 NIMBUS 2 DEB
1 28617U 66040AG  26125.43390962  .00003798  00000-0  36001-2 0  9991
2 28617 100.4753   0.1689 0045135 155.9493  22.4194 13.81258415189147

Epoch: 2026-05-05T10:24Z

TLE epoch observation values (Epoch: 2026-05-05T10:24:49.791Z)

Latitude

1.30375°

Longitude

160.89246°

Altitude

931.469 km

Speed

7.402 km/s

True Right ascension

12h 01m 38s

True Declination

1° 17' 46"

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

19:11:03

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

989.834 km

Perigee altitude

923.622 km

Semi-major axis

7,334.865 km

Eccentricity

0.00451

Inclination

100.4753°

RAAN

0.1689°

Arg. of periapsis

155.9493°

True anomaly

22.61769°

Mean anomaly

22.4194°

Eccentric anomaly

22.51844°

Mean motion

3.45505 °/min

Orbital period

104.2 mins

BSTAR

0.0036001

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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.
8 mins	2026-05-08 14:12:21.537Z	104.843° ESE	2026-05-08 14:16:21.537Z	58.414° ENE	21.237°	2026-05-08 14:20:21.537Z	13.846° NNE
10 mins	2026-05-08 15:54:21.537Z	183.926° SSW	2026-05-08 15:58:21.537Z	251.841° W	40.285°	2026-05-08 16:04:21.537Z	335.989° NNW
9 mins	2026-05-09 04:33:21.537Z	20.329° NNE	2026-05-09 04:37:21.537Z	86.19° E	44.37°	2026-05-09 04:42:21.537Z	191.493° SSW
5 mins	2026-05-09 06:17:21.537Z	327.567° NNW	2026-05-09 06:19:21.537Z	304.7° NW	15.694°	2026-05-09 06:22:21.537Z	271.336° WNW

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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, 28617 on other resources

View NIMBUS 2 DEB, 28617 on Heavens-Above

View NIMBUS 2 DEB, 28617 on Keep Track

View NIMBUS 2 DEB, 28617 on Celestrak

View NIMBUS 2 DEB, 28617 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, 28617

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-05-05T10:24:49.791Z)

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, 28617 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago