DUMMY MASS 2

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite DUMMY MASS 2 at a glance.

Uptime

10235

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 2.

Object identification

Identified? True

Debris? False

Object name: DUMMY MASS 2

International designator: 1997-048B

Object number (NORAD): 24926

Object ID (CCSDS): 24926

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 96.852 minutes

Inclination: 86.3297 deg

SMA: 6986.08 km

Apoapsis: 612.156 km

Periapsis: 603.734 km

RAAN: 98.3899 deg

Eccentricy: 0.00060274

Argument of periapsis: 206.2713 deg

Mean anomaly: 153.8207 deg

Mean motion: 14.86799651 rev/day

Mean motion (dot): 0.00000458 rev/day2

B* drag term: 0.000048198866 1/REarth

Two-line elements (TLE)

Creation date: Sept. 8, 2025, 6:18 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Sept. 8, 2025, 1:37 p.m. UTC

TLE line 0: 0 DUMMY MASS 2

TLE line 1: 1 24926U 97048B 25251.56789961 .00000458 00000-0 48199-4 0 9999

TLE line 2: 2 24926 86.3297 98.3899 0006027 206.2713 153.8207 14.86799651517298

Live tracking on map

Real-time ground track for satellite DUMMY MASS 2.

In-orbit conjunctions

A list of the most updated potential collisions computed for object DUMMY MASS 2.

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 2251 DEB LEO 2025-07-18 20:45:10 0.0001879837 466.0 (m) DEBRIS
CZ-2C DEB SSO 2024-07-08 15:48:27 0.001297747 333.0 (m) DEBRIS
COSMOS 1275 DEB LEO 2024-06-01 08:54:38 0.0001067406 821.0 (m) DEBRIS

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 2 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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