DUMSAT

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite DUMSAT at a glance.

Uptime

9221

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: 96.203 minutes

Inclination: 64.852 deg

SMA: 6954.81 km

Apoapsis: 592.513 km

Periapsis: 560.838 km

RAAN: 254.5308 deg

Eccentricy: 0.0022772

Argument of periapsis: 277.3706 deg

Mean anomaly: 82.4822 deg

Mean motion: 14.96838077 rev/day

Mean motion (dot): 0.00000396 rev/day2

B* drag term: 0.000048532 1/REarth

Two-line elements (TLE)

Creation date: May 8, 2025, 3:01 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 7, 2025, 5:28 p.m. UTC

TLE line 0: 0 DUMSAT

TLE line 1: 1 26086U 00009A 25127.72825540 .00000396 00000-0 48532-4 0 9995

TLE line 2: 2 26086 64.8520 254.5308 0022772 277.3706 82.4822 14.96838077377543

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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