SL-24 R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite SL-24 R/B at a glance.

Uptime

5762

Days in orbit

Revolutions

≈ 13.7

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.1

Latest

Satellite identification and parameters

Extended collection of information and parameters for SL-24 R/B.

Object identification

Identified? True

Debris? False

Object name: SL-24 R/B

International designator: 2009-041H

Object number (NORAD): 35688

Object ID (CCSDS): 35688

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 104.764 minutes

Inclination: 98.0908 deg

SMA: 7361.52 km

Apoapsis: 1299.065 km

Periapsis: 667.704 km

RAAN: 339.0221 deg

Eccentricy: 0.0428825

Argument of periapsis: 342.797 deg

Mean anomaly: 148.6448 deg

Mean motion: 13.74521505 rev/day

Mean motion (dot): 0.0000002 rev/day2

B* drag term: 0.000031616 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, 10:28 p.m. UTC

TLE line 0: 0 SL-24 R/B

TLE line 1: 1 35688U 09041H 25127.93648021 .00000020 00000-0 31616-4 0 9997

TLE line 2: 2 35688 98.0908 339.0221 0428825 342.7970 148.6448 13.74521505791170

Live tracking on map

Real-time ground track for satellite SL-24 R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object SL-24 R/B.

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 1275 DEB LEO 2025-03-03 20:29:00 0.0002072382 78.0 (m) DEBRIS
METEOR 2-8 DEB LEO 2024-10-02 03:57:37 0.0001451013 248.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-09-07 13:44:37 0.001717357 184.0 (m) DEBRIS
SPOT 4 SSO 2024-08-20 19:15:46 0.0005049183 510.0 (m) PAYLOAD

Associated space launch

Emirati Earth observation satellite. Launched with 5 secondary payloads.

SL-24 R/B was lifted into orbit during the mission ‘Dnepr | DubaiSat 1’, on board a Dnepr space rocket.

The launch took place on July 29, 2009, 6:46 p.m. from 109/95.

For more information about the launch, click the button.

Launch to space Dnepr | DubaiSat 1
Dnepr | DubaiSat 1

Agency: N/A

Status: Launch Successful

Launch date: July 29, 2009, 6:46 p.m. UTC

Rocket: Dnepr

Launch pad: 109/95

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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