GEISAT PRECURSOR
NORAD 56934
Payload
LEO
2023-084C
● Active
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LEO · NORAD 56934
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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
459 km
Apogee
465 km
Inclination
97.6°
Period
93.8 min
Mean Motion
15.34681643 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude462 km
Orbital Velocity27,496 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.35
Eccentricity0.0004
Semi-Major Axis6,833 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇪🇸 Spain
Launch Date
2023-06-12
Launch Site
Vandenberg SFB, California
Int'l Designator
2023-084C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
GEISAT PRECURSOR is an active satellite operated by Spain, launched on 2023-06-12 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 459 km and 465 km with an inclination of 97.6°. It travels at approximately 27,496 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.35 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 ~1–3 years. Orbital Radar tracks GEISAT PRECURSOR in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GEISAT PRECURSOR orbits at an average altitude of 462 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 GEISAT PRECURSOR’s average altitude, there are currently 7,988 active payloads and 175 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 45.8% of all active satellites. With an inclination of 97.6°, GEISAT PRECURSOR passes over latitudes between 97.6°N and 97.6°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. Spain operates approximately 53 active satellites in total, of which 23 share a similar altitude band with GEISAT PRECURSOR.
❓ Frequently Asked Questions
GEISAT PRECURSOR is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 462 km altitude. Its 97.6° 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 94 minutes, travelling at 27,496 km/h.
GEISAT PRECURSOR is operated by Spain. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 56934. You can track GEISAT PRECURSOR in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GEISAT PRECURSOR was launched on 2023-06-12 from Vandenberg SFB, California, 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks GEISAT PRECURSOR (NORAD ID 56934) 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.
GEISAT PRECURSOR travels at approximately 27,496 km/h (17,085 mph) — roughly 7.64 km/s. It completes 15.35 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.