GEMINI-POLLUX
NORAD 69000
Payload
LEO
2026-100W
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LEO · NORAD 69000
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
588 km
Apogee
591 km
Inclination
97.7°
Period
96.5 min
Mean Motion
14.92691664 rev/day
TLE Epoch
2026-11-03 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude590 km
Orbital Velocity27,243 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.93
Eccentricity0.0002
Semi-Major Axis6,961 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
NCKU (TWN)
Launch Date
2026-05-03
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2026-100W
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
GEMINI-POLLUX is an active satellite operated by NCKU (TWN), launched on 2026-05-03 from Vandenberg Space Force Base, United States on the RideshareX-2026-100 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 588 km and 591 km with an inclination of 97.7°. It travels at approximately 27,243 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.93 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. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks GEMINI-POLLUX in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GEMINI-POLLUX orbits at an average altitude of 590 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 GEMINI-POLLUX’s average altitude, there are currently 1,527 active payloads and 663 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3055. This makes it one of the more crowded altitude bands, containing roughly 7.8% of all active satellites. With an inclination of 97.7°, GEMINI-POLLUX 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. TWN operates approximately 34 active satellites in total, of which 15 share a similar altitude band with GEMINI-POLLUX.
❓ Frequently Asked Questions
GEMINI-POLLUX is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 590 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 96 minutes, travelling at 27,243 km/h.
GEMINI-POLLUX is operated by NCKU (TWN). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 69000. You can track GEMINI-POLLUX in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GEMINI-POLLUX was launched on 2026-05-03 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks GEMINI-POLLUX (NORAD ID 69000) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
GEMINI-POLLUX travels at approximately 27,243 km/h (16,928 mph) — roughly 7.57 km/s. It completes 14.93 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.