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VIKING

NORAD 16614 Payload MEO 1986-019B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
815 km
Apogee
13523 km
Inclination
98.8°
Period
261.5 min
Mean Motion
5.50603748 rev/day
TLE Epoch
2026-06-18 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude7,169 km
Orbital Velocity19,533 km/h
Velocity5.43 km/s
Orbital Period4 hours 22 minutes
Orbits / Day5.51
Eccentricity0.4693
Semi-Major Axis13,540 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇸🇪 Sweden
Launch Date
1986-02-22
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1986-019B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
VIKING is an active satellite operated by Sweden, launched on 1986-02-22 from Guiana Space Centre, Kourou. With over 40 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 815 km and 13,523 km with an inclination of 98.8°. It travels at approximately 19,533 km/h (5.43 km/s), completing one full orbit every 4 hours 22 minutes — that’s roughly 5.51 orbits per day. Its orbital eccentricity of 0.4693 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks VIKING in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
VIKING orbits at an average altitude of 7,169 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of VIKING’s average altitude, there are currently 2 active payloads and 7 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 98.8°, VIKING passes over latitudes between 98.8°N and 98.8°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Sweden operates approximately 15 active satellites in total.
❓ Frequently Asked Questions
VIKING orbits in Medium Earth Orbit (MEO) at altitudes between 815 km (perigee) and 13,523 km (apogee), with an average altitude of approximately 7,169 km. It completes one orbit every 4 hours 22 minutes, travelling at approximately 19,533 km/h (12,137 mph).
VIKING is operated by Sweden. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 16614. You can track VIKING in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
VIKING was launched on 1986-02-22 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks VIKING (NORAD ID 16614) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
VIKING travels at approximately 19,533 km/h (12,137 mph) — roughly 5.43 km/s. It completes 5.51 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 11 sunrises and sunsets every 24 hours.