DUMSAT

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite DUMSAT at a glance.

Uptime

9385

Days in orbit

Revolutions

≈ 15.0

Per day

Orbit

LEO

Low Earth Orbit

Inclination

64.9

Latest

Satellite identification and parameters

Extended collection of information and parameters for DUMSAT.

Object identification

Identified? True

Debris? False

Object name: DUMSAT

International designator: 2000-009A

Object number (NORAD): 26086

Object ID (CCSDS): 26086

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 96.194 minutes

Inclination: 64.85 deg

SMA: 6954.374 km

Apoapsis: 593.157 km

Periapsis: 559.322 km

RAAN: 101.0854 deg

Eccentricy: 0.00243266

Argument of periapsis: 270.0544 deg

Mean anomaly: 89.7784 deg

Mean motion: 14.96978899 rev/day

Mean motion (dot): 0.00000535 rev/day2

B* drag term: 0.000060326281 1/REarth

Two-line elements (TLE)

Creation date: Oct. 19, 2025, 2:20 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 18, 2025, 10:41 p.m. UTC

TLE line 0: 0 DUMSAT

TLE line 1: 1 26086U 00009A 25291.94551700 .00000535 00000-0 60326-4 0 9995

TLE line 2: 2 26086 64.8500 101.0854 0024327 270.0544 89.7784 14.96978899402128

Live tracking on map

Real-time ground track for satellite DUMSAT.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB LEO 2024-10-29 23:17:26 0.0004019174 344.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-08-25 20:10:42 0.0001464491 784.0 (m) DEBRIS

Associated space launch

IRDT (Inflatable Re-Entry and Descent Technology) is a new technology to return payloads from orbit without a heavy heatshield and parachute system. A inflatable cone provides protection during reentry and a second inflatable extension of the cone reduces the speed further for a safe landing.

DUMSAT was lifted into orbit during the mission ‘Soyuz-U-PVB | IRDT 1’, on board a Soyuz-U-PVB space rocket.

The launch took place on Feb. 8, 2000, 11:20 p.m. from 31/6.

For more information about the launch, click the button.

Launch to space Soyuz-U-PVB | IRDT 1
Soyuz-U-PVB | IRDT 1

Agency: N/A

Status: Launch Successful

Launch date: Feb. 8, 2000, 11:20 p.m. UTC

Rocket: Soyuz-U-PVB

Launch pad: 31/6

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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