SL-16 DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite SL-16 DEB at a glance.

Uptime

9487

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

97.7

Latest

Satellite identification and parameters

Extended collection of information and parameters for SL-16 DEB.

Object identification

Identified? True

Debris? True

Object name: SL-16 DEB

International designator: 1999-039C

Object number (NORAD): 25862

Object ID (CCSDS): 25862

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.76 minutes

Inclination: 97.7036 deg

SMA: 7125.198 km

Apoapsis: 860.303 km

Periapsis: 633.824 km

RAAN: 193.7373 deg

Eccentricy: 0.0158928

Argument of periapsis: 110.9474 deg

Mean anomaly: 250.8808 deg

Mean motion: 14.43468602 rev/day

Mean motion (dot): 0.00000697 rev/day2

B* drag term: 0.00018748 1/REarth

Two-line elements (TLE)

Creation date: July 6, 2025, 6:05 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 1:21 p.m. UTC

TLE line 0: 0 SL-16 DEB

TLE line 1: 1 25862U 99039C 25187.55628672 .00000697 00000-0 18748-3 0 9990

TLE line 2: 2 25862 97.7036 193.7373 0158928 110.9474 250.8808 14.43468602362920

Live tracking on map

Real-time ground track for satellite SL-16 DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object SL-16 DEB.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB LEO 2024-11-09 10:50:10 0.000152973 543.0 (m) DEBRIS

Associated space launch

Okean-O was a joint Ukrainian and Russian remote sensing satellite program designed as a follow on to the Okean-O1 series. It was designed to gather remote sensing data crucial for research of natural resources of the Earth and world oceans. The mission also included ecological monitoring and management of externalities (weather forecast, hazards prevention).

SL-16 DEB was lifted into orbit during the mission ‘Zenit-2 | Okean-O’, on board a Zenit-2 space rocket.

The launch took place on July 17, 1999, 5:38 a.m. from 45/1.

For more information about the launch, click the button.

Launch to space Zenit-2 | Okean-O
Zenit-2 | Okean-O

Agency: N/A

Status: Launch Successful

Launch date: July 17, 1999, 5:38 a.m. UTC

Rocket: Zenit-2

Launch pad: 45/1

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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