Key statistics
Satellite OKEAN O at a glance.
Uptime
9483
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 OKEAN O.
Object identification
Identified? True
Debris? False
Object name: OKEAN O
International designator: 1999-039A
Object number (NORAD): 25860
Object ID (CCSDS): 25860
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 97.309 minutes
Inclination: 97.9824 deg
SMA: 7008.011 km
Apoapsis: 631.237 km
Periapsis: 628.515 km
RAAN: 240.6161 deg
Eccentricy: 0.0001942
Argument of periapsis: 84.9439 deg
Mean anomaly: 275.1994 deg
Mean motion: 14.79825707 rev/day
Mean motion (dot): 0.00000522 rev/day2
B* drag term: 0.000076259 1/REarth
Two-line elements (TLE)
Creation date: July 3, 2025, 3:40 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 2, 2025, 5:08 p.m. UTC
TLE line 0: 0 OKEAN O
TLE line 1: 1 25860U 99039A 25183.71419673 .00000522 00000-0 76259-4 0 9990
TLE line 2: 2 25860 97.9824 240.6161 0001942 84.9439 275.1994 14.79825707397416
Live tracking on map
Real-time ground track for satellite OKEAN O.
In-orbit conjunctions
A list of the most updated potential collisions computed for object OKEAN O.
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).
OKEAN O 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.
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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