ARIANE 2 DEB, 26728

Orbit data source: Space-Track

ARIANE 2 DEB, 26728 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/26728?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

Identifier

26728, 1989-006F

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, 1.1 m

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago

0 ARIANE 2 DEB
1 26728U 89006F   25349.63574919  .00003299  00000-0  97201-2 0  9999
2 26728   8.1149 287.0980 7047482  16.2618 357.8524  2.48203808215603

Epoch: 2025-12-15T15:15Z

TLE epoch observation values (Epoch: 2025-12-15T15:15:28.730Z)

Latitude

0.00019°

Longitude

-26.22487°

Altitude

537.988 km

Speed

9.897 km/s

True Right ascension

19h 08m 42s

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

11:16:33

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

32,912.396 km

Perigee altitude

426.739 km

Semi-major axis

23,047.705 km

Eccentricity

0.70475

Inclination

8.1149°

RAAN

287.098°

Arg. of periapsis

16.2618°

True anomaly

342.7404°

Mean anomaly

357.8524°

Eccentric anomaly

352.77193°

Mean motion

0.6203 °/min

Orbital period

580.36 mins

BSTAR

0.0097201

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

ARIANE 2 DEB, 27035 (Decayed)

ARIANE 2 DEB, 27031

ARIANE 2 DEB, 40788

ARIANE 2 DEB, 28570

ARIANE 2 DEB, 27044

ARIANE 2 DEB, 27650

ARIANE 2 DEB, 33567

ARIANE 2 DEB, 33551

ARIANE 2 DEB, 33548

ARIANE 2 DEB, 33565

ARIANE 2 DEB, 27046

ARIANE 2 DEB, 29023

ARIANE 2 DEB, 27029

ARIANE 2 DEB, 28566

ARIANE 2 DEB, 27039

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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.
367 mins	2025-12-17 06:28:24.113Z	238.8° WSW	2025-12-17 08:12:24.113Z	192.888° SSW	33.785°	2025-12-17 12:35:24.113Z	218.059° SW

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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 ARIANE 2 DEB, 26728 on other resources

View ARIANE 2 DEB, 26728 on Heavens-Above

View ARIANE 2 DEB, 26728 on Keep Track

View ARIANE 2 DEB, 26728 on Celestrak

View ARIANE 2 DEB, 26728 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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