VRSS-2
NORAD 42954
Payload
LEO
2017-060A
● Active
CONNECTING…
LEO · NORAD 42954
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
612 km
Apogee
639 km
Inclination
97.7°
Period
97.2 min
Mean Motion
14.81199302 rev/day
TLE Epoch
2026-06-19 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude626 km
Orbital Velocity27,173 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.81
Eccentricity0.0019
Semi-Major Axis6,997 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
Bolivarian Agency for Space Activities (Venezuela)
Launch Date
2017-10-09
Launch Site
Jiuquan, China
Int'l Designator
2017-060A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
VRSS-2 is an active satellite operated by Bolivarian Agency for Space Activities (Venezuela), launched on 2017-10-09 from Jiuquan, China. It orbits in Low Earth Orbit (LEO) at altitudes between 612 km and 639 km with an inclination of 97.7°. It travels at approximately 27,173 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.81 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks VRSS-2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
VRSS-2 orbits at an average altitude of 626 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of VRSS-2’s average altitude, there are currently 805 active payloads and 809 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050. With an inclination of 97.7°, VRSS-2 passes over latitudes between 97.7°N and 97.7°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. Venezuela operates approximately 3 active satellites in total, of which 2 share a similar altitude band with VRSS-2.
❓ Frequently Asked Questions
VRSS-2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 626 km altitude. Its 97.7° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 97 minutes, travelling at 27,173 km/h.
VRSS-2 is operated by Bolivarian Agency for Space Activities (Venezuela). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 42954. You can track VRSS-2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
VRSS-2 was launched on 2017-10-09 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks VRSS-2 (NORAD ID 42954) 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.
VRSS-2 travels at approximately 27,173 km/h (16,884 mph) — roughly 7.55 km/s. It completes 14.81 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.