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

9488

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: 97.212 minutes

Inclination: 98.0348 deg

SMA: 7003.342 km

Apoapsis: 635.192 km

Periapsis: 615.223 km

RAAN: 242.7994 deg

Eccentricy: 0.0014257

Argument of periapsis: 336.4127 deg

Mean anomaly: 23.643 deg

Mean motion: 14.8130582 rev/day

Mean motion (dot): 0.00000381 rev/day2

B* drag term: 0.000055688 1/REarth

Two-line elements (TLE)

Creation date: July 8, 2025, 2:27 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 7, 2025, 8:49 p.m. UTC

TLE line 0: 0 SL-16 R/B

TLE line 1: 1 25861U 99039B 25188.86782208 .00000381 00000-0 55688-4 0 9995

TLE line 2: 2 25861 98.0348 242.7994 0014257 336.4127 23.6430 14.81305820400619

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
OBJECT C SSO 2025-05-15 22:12:08 0.002085755 61.0 (m) UNKNOWN
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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