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ARIANE 2 DEB, 28565

Orbit data source: Space-Track

ARIANE 2 DEB, 28565 is space debris in HEO originally from a launch on Fri, 27 Jan 1989 UTC launched from the French Guiana (FRGUI). 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/28565?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

Identifier

28565, 1989-006AG

Orbit

HEO

Country

FR

Related business

ArianeGroup (FR)

Manufacturer

EADS/LV

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1989-01-27 (37 years ago)

Launch vehicle

Unknown

Launch site

French Guiana (FRGUI)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.3 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 6 days ago

TLE from 6 days ago

0 ARIANE 2 DEB
1 28565U 89006AG  26066.31371762  .00000019  00000-0  53130-3 0  9994
2 28565   8.6440 347.4698 7081526 253.9092  23.3342  2.39486848188163

Epoch: 2026-03-07T07:31Z

TLE epoch observation values (Epoch: 2026-03-07T07:31:45.202Z)

Latitude

0.00028°

Longitude

69.49577°

Altitude

8,302.987 km

Speed

6.116 km/s

True Right ascension

23h 09m 53s

True Declination

0° 00' 01"

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

11:28:51

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

33,940.138 km

Perigee altitude

510.465 km

Semi-major axis

23,603.438 km

Eccentricity

0.70815

Inclination

8.644°

RAAN

347.4698°

Arg. of periapsis

253.9092°

True anomaly

106.10831°

Mean anomaly

23.3342°

Eccentric anomaly

57.58726°

Mean motion

0.59852 °/min

Orbital period

601.48 mins

BSTAR

0.0005313

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Computing Atmospheric mass density...

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Other satellites on launch #6 in the year 1989 (1989-01-27 UTC)

ARIANE 2 DEB, 27046

ARIANE 2 DEB, 27029

ARIANE 2 DEB, 28566

ARIANE 2 DEB, 29023

ARIANE 2 DEB, 42484

ARIANE 2 DEB, 33549

ARIANE 2 DEB, 33569

ARIANE 2 DEB, 40787

ARIANE 2 DEB, 33574

ARIANE 2 DEB, 28567

ARIANE 2 DEB, 28569

ARIANE 2 DEB, 33555

ARIANE 2 DEB, 27041

ARIANE 2 DEB, 33564

ARIANE 2 DEB, 28564

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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

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ARIANE 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.
282 mins	2026-03-14 00:27:35.724Z	252.001° W	2026-03-14 02:00:35.724Z	251.367° W	20.291°	2026-03-14 05:09:35.724Z	265.005° W

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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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Click to sort rows by RSO header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Type header in ascending order	Click to sort rows by Inclination Δ header in ascending order	Click to sort rows by RAAN Δ header in ascending order	Click to sort rows by Coplanar Angle header in ascending order	Click to sort rows by SMA Δ header in ascending order	Click to sort rows by Orbital period header in ascending order	Click to sort rows by <5km Md TCA header in descending order

CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out ARIANE 2 DEB, 28565 on other resources

View ARIANE 2 DEB, 28565 on Heavens-Above

View ARIANE 2 DEB, 28565 on Keep Track

View ARIANE 2 DEB, 28565 on Celestrak

View ARIANE 2 DEB, 28565 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

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