SAOCOM 1-A
NORAD 43641
Payload
LEO
2018-076A
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LEO · NORAD 43641
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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
621 km
Apogee
624 km
Inclination
97.9°
Period
97.2 min
Mean Motion
14.82150752 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude623 km
Orbital Velocity27,178 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.82
Eccentricity0.0002
Semi-Major Axis6,994 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
National Space Activities Commission (CONAE) (Argentina)
Launch Date
2018-10-08
Launch Site
Vandenberg SFB, California
Int'l Designator
2018-076A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SAOCOM 1-A is an active satellite operated by National Space Activities Commission (CONAE) (Argentina), launched on 2018-10-08 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 621 km and 624 km with an inclination of 97.9°. It travels at approximately 27,178 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.82 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 ~10–25 years. Orbital Radar tracks SAOCOM 1-A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SAOCOM 1-A orbits at an average altitude of 623 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 SAOCOM 1-A’s average altitude, there are currently 833 active payloads and 791 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3055, STARLINK-3109. With an inclination of 97.9°, SAOCOM 1-A passes over latitudes between 97.9°N and 97.9°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. Argentina operates approximately 34 active satellites in total, of which 7 share a similar altitude band with SAOCOM 1-A.
❓ Frequently Asked Questions
SAOCOM 1-A is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 623 km altitude. Its 97.9° 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 27,178 km/h.
SAOCOM 1-A is operated by National Space Activities Commission (CONAE) (Argentina). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43641. You can track SAOCOM 1-A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SAOCOM 1-A was launched on 2018-10-08 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks SAOCOM 1-A (NORAD ID 43641) 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.
SAOCOM 1-A travels at approximately 27,178 km/h (16,888 mph) — roughly 7.55 km/s. It completes 14.82 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.