SL-16 R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite SL-16 R/B at a glance.

Uptime

9428

Days in orbit

Revolutions

≈ 14.8

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.0

Latest

Satellite identification and parameters

Extended collection of information and parameters for SL-16 R/B.

Object identification

Identified? True

Debris? False

Object name: SL-16 R/B

International designator: 1999-039B

Object number (NORAD): 25861

Object ID (CCSDS): 25861

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 97.216 minutes

Inclination: 98.0388 deg

SMA: 7003.572 km

Apoapsis: 636.236 km

Periapsis: 614.638 km

RAAN: 182.5107 deg

Eccentricy: 0.0015419

Argument of periapsis: 161.1323 deg

Mean anomaly: 199.0463 deg

Mean motion: 14.8123288 rev/day

Mean motion (dot): 0.00000831 rev/day2

B* drag term: 0.00011352 1/REarth

Two-line elements (TLE)

Creation date: May 9, 2025, 2:46 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 8, 2025, 5:56 p.m. UTC

TLE line 0: 0 SL-16 R/B

TLE line 1: 1 25861U 99039B 25128.74786340 .00000831 00000-0 11352-3 0 9996

TLE line 2: 2 25861 98.0388 182.5107 0015419 161.1323 199.0463 14.81232880391711

Live tracking on map

Real-time ground track for satellite SL-16 R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object SL-16 R/B.

Target Orbit TCA Probability of collision Miss distance Type
SL-14 R/B LEO 2025-03-13 02:51:42 0.000279672 435.0 (m) ROCKET BODY
ELECTRON KICK STAGE R/B LEO 2024-09-20 12:12:14 0.0001551539 597.0 (m) ROCKET BODY

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 R/B 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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