DEMETER

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite DEMETER at a glance.

Uptime

7678

Days in orbit

Revolutions

≈ 14.8

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.1

Latest

Satellite identification and parameters

Extended collection of information and parameters for DEMETER.

Object identification

Identified? True

Debris? False

Object name: DEMETER

International designator: 2004-025C

Object number (NORAD): 28368

Object ID (CCSDS): 28368

Country: FRANCE (FR)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 97.159 minutes

Inclination: 98.0829 deg

SMA: 7000.798 km

Apoapsis: 623.915 km

Periapsis: 621.41 km

RAAN: 157.8623 deg

Eccentricy: 0.0001789

Argument of periapsis: 112.2938 deg

Mean anomaly: 247.8464 deg

Mean motion: 14.82113493 rev/day

Mean motion (dot): 0.00001208 rev/day2

B* drag term: 0.00015866 1/REarth

Two-line elements (TLE)

Creation date: July 6, 2025, 10:46 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 9:41 p.m. UTC

TLE line 0: 0 DEMETER

TLE line 1: 1 28368U 04025C 25187.90385403 .00001208 00000-0 15866-3 0 9993

TLE line 2: 2 28368 98.0829 157.8623 0001789 112.2938 247.8464 14.82113493129506

Live tracking on map

Real-time ground track for satellite DEMETER.

In-orbit conjunctions

A list of the most updated potential collisions computed for object DEMETER.

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 2251 DEB LEO 2025-05-16 10:58:55 0.000295392 69.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-04-13 03:33:47 0.0001423089 703.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2024-12-19 20:18:14 0.0001340472 685.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-11-11 05:52:42 0.003508834 318.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2024-09-09 21:21:54 0.000484065 136.0 (m) DEBRIS

Associated space launch

AprizeSat, is a constellation of small Low-Earth-Orbit satellites (64 satellites planned) to achieve a global communication system of data transmission and fixed and mobile asset tracking and monitoring (GMPCS).

DEMETER was lifted into orbit during the mission ‘Dnepr | Aprizesat-2’, on board a Dnepr space rocket.

The launch took place on June 29, 2004, 6:30 a.m. from 109/95.

For more information about the launch, click the button.

Launch to space Dnepr | Aprizesat-2
Dnepr | Aprizesat-2

Agency: N/A

Status: Launch Successful

Launch date: June 29, 2004, 6:30 a.m. UTC

Rocket: Dnepr

Launch pad: 109/95

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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