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

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 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: 96.848 minutes

Inclination: 86.3319 deg

SMA: 6985.875 km

Apoapsis: 614.329 km

Periapsis: 601.151 km

RAAN: 76.4825 deg

Eccentricy: 0.00094318

Argument of periapsis: 63.2672 deg

Mean anomaly: 296.9517 deg

Mean motion: 14.8686502 rev/day

Mean motion (dot): 0.00000726 rev/day2

B* drag term: 0.000078206426 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, 9:08 p.m. UTC

TLE line 0: 0 DUMMY MASS 2

TLE line 1: 1 24926U 97048B 25298.88110577 .00000726 00000-0 78206-4 0 9996

TLE line 2: 2 24926 86.3319 76.4825 0009432 63.2672 296.9517 14.86865020524326

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
CZ-6A DEB SSO 2025-09-20 16:49:13 0.000279399 312.0 (m) DEBRIS
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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