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

5820

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: 104.763 minutes

Inclination: 98.0857 deg

SMA: 7361.5 km

Apoapsis: 1299.183 km

Periapsis: 667.547 km

RAAN: 28.0449 deg

Eccentricy: 0.0429013

Argument of periapsis: 185.3203 deg

Mean anomaly: 189.1249 deg

Mean motion: 13.74526929 rev/day

Mean motion (dot): 0.00000011 rev/day2

B* drag term: 0.000025292 1/REarth

Two-line elements (TLE)

Creation date: July 4, 2025, 6:39 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 4, 2025, 1:32 p.m. UTC

TLE line 0: 0 SL-24 R/B

TLE line 1: 1 35688U 09041H 25185.56452448 .00000011 00000-0 25292-4 0 9999

TLE line 2: 2 35688 98.0857 28.0449 0429013 185.3203 189.1249 13.74526929799093

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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