ARIANE 42P DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite ARIANE 42P DEB at a glance.

Uptime

12021

Days in orbit

Revolutions

≈ 12.9

Per day

Orbit

LEO

Low Earth Orbit

Inclination

66.0

Latest

Satellite identification and parameters

Extended collection of information and parameters for ARIANE 42P DEB.

Object identification

Identified? True

Debris? True

Object name: ARIANE 42P DEB

International designator: 1992-052E

Object number (NORAD): 44507

Object ID (CCSDS): 44507

Country: FRANCE (FR)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 111.836 minutes

Inclination: 66.0072 deg

SMA: 7689.2 km

Apoapsis: 1412.792 km

Periapsis: 1209.338 km

RAAN: 235.6428 deg

Eccentricy: 0.0132299

Argument of periapsis: 93.0574 deg

Mean anomaly: 268.5592 deg

Mean motion: 12.8760021 rev/day

Mean motion (dot): 0.00001716 rev/day2

B* drag term: 0.0067702 1/REarth

Two-line elements (TLE)

Creation date: July 8, 2025, 5:26 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 8, 2025, 12:54 p.m. UTC

TLE line 0: 0 ARIANE 42P DEB

TLE line 1: 1 44507U 92052E 25189.53781765 .00001716 00000-0 67702-2 0 9994

TLE line 2: 2 44507 66.0072 235.6428 0132299 93.0574 268.5592 12.87600210276624

Live tracking on map

Real-time ground track for satellite ARIANE 42P DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object ARIANE 42P DEB.

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 1800 LEO 2025-02-06 19:20:45 0.0005938089 362.0 (m) PAYLOAD

Associated space launch

The TOPEX/POSEIDON satellite was launched on 10 August 1992 with the objective of "observing and understanding the ocean circulation". A joint project between NASA, the U.S. space agency, and CNES, the French space agency, it carries two radar altimeters and precise orbit determination systems, including the DORIS system. KITSAT-1 (Korean Institute of Technology Satellite) was a collaborative research mission, encompassing the installation of a groundstation in South Korea, participation of Korean engineers in the UoSAT-5 mission, technology transfer and training of students on the MSc courses at Surrey, and the involvement in a engineering and flight microsatellites. The S80/T satellite was built for CNES by Matra Marconi Space using the Surrey Satellite Technology Microbus (Uosat) bus.

ARIANE 42P DEB was lifted into orbit during the mission ‘Ariane 42P | Topex-Poseidon, Kitsat 1 & S80/T’, on board a Ariane 42P space rocket.

The launch took place on Aug. 10, 1992, 11:08 p.m. from Ariane Launch Area 2.

For more information about the launch, click the button.

Launch to space Ariane 42P | Topex-Poseidon, Kitsat 1 & S80/T
Ariane 42P | Topex-Poseidon, Kitsat 1 & S80/T

Agency: N/A

Status: Launch Successful

Launch date: Aug. 10, 1992, 11:08 p.m. UTC

Rocket: Ariane 42P

Launch pad: Ariane Launch Area 2

Location: Guiana Space Centre, French Guiana

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