DUMMY MASS 1

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite DUMMY MASS 1 at a glance.

Uptime

10282

Days in orbit

Revolutions

≈ 14.9

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.3

Latest

Satellite identification and parameters

Extended collection of information and parameters for DUMMY MASS 1.

Object identification

Identified? True

Debris? False

Object name: DUMMY MASS 1

International designator: 1997-048A

Object number (NORAD): 24925

Object ID (CCSDS): 24925

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 96.832 minutes

Inclination: 86.3321 deg

SMA: 6985.095 km

Apoapsis: 612.843 km

Periapsis: 601.077 km

RAAN: 74.8424 deg

Eccentricy: 0.00084219

Argument of periapsis: 54.8584 deg

Mean anomaly: 305.3429 deg

Mean motion: 14.87114161 rev/day

Mean motion (dot): 0.00000737 rev/day2

B* drag term: 0.000078966951 1/REarth

Two-line elements (TLE)

Creation date: Oct. 26, 2025, 2:54 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 25, 2025, 9:31 p.m. UTC

TLE line 0: 0 DUMMY MASS 1

TLE line 1: 1 24925U 97048A 25298.89714303 .00000737 00000-0 78967-4 0 9999

TLE line 2: 2 24925 86.3321 74.8424 0008422 54.8584 305.3429 14.87114161524557

Live tracking on map

Real-time ground track for satellite DUMMY MASS 1.

In-orbit conjunctions

A list of the most updated potential collisions computed for object DUMMY MASS 1.

Target Orbit TCA Probability of collision Miss distance Type
H-2A DEB SSO 2024-12-12 00:52:06 0.0004545326 826.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-11 17:46:45 0.0001676873 93.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2024-09-26 13:50:16 0.0002542778 206.0 (m) DEBRIS
SL-14 R/B LEO 2024-09-14 06:40:31 0.0008760614 320.0 (m) ROCKET BODY

Associated space launch

The Iridium-MFS payloads were mass models of the Iridium communications satellites. Two were launched to test the new CZ-2C (2) SD launch vehicle and the payload dispenser.

DUMMY MASS 1 was lifted into orbit during the mission ‘Long March 2C/SD | Iridium MFS 1 & 2’, on board a Long March 2C/SD space rocket.

The launch took place on Sept. 1, 1997, 2 p.m. from Launch Complex 7.

For more information about the launch, click the button.

Launch to space Long March 2C/SD | Iridium MFS 1 & 2
Long March 2C/SD | Iridium MFS 1 & 2

Agency: N/A

Status: Launch Successful

Launch date: Sept. 1, 1997, 2 p.m. UTC

Rocket: Long March 2C/SD

Launch pad: Launch Complex 7

Location: Taiyuan Satellite Launch Center, People's Republic of China

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