Skip to content
Home Library Satellite Directory APEX ARIES 1

APEX ARIES 1

NORAD 59129 Payload LEO 2024-043AH ● Active
CONNECTING… LEO · NORAD 59129
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
396 km
Apogee
403 km
Inclination
97.5°
Period
92.5 min
Mean Motion
15.55878375 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude400 km
Orbital Velocity27,622 km/h
Velocity7.67 km/s
Orbital Period93 minutes
Orbits / Day15.56
Eccentricity0.0005
Semi-Major Axis6,771 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2024-03-04
Launch Site
Vandenberg SFB, California
Int'l Designator
2024-043AH
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
APEX ARIES 1 is an active satellite operated by United States, launched on 2024-03-04 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 396 km and 403 km with an inclination of 97.5°. It travels at approximately 27,622 km/h (7.67 km/s), completing one full orbit every 93 minutes — that’s roughly 15.56 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 months to ~1 year. Orbital Radar tracks APEX ARIES 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
APEX ARIES 1 orbits at an average altitude of 400 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 APEX ARIES 1’s average altitude, there are currently 1,329 active payloads and 92 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 7.6% of all active satellites. With an inclination of 97.5°, APEX ARIES 1 passes over latitudes between 97.5°N and 97.5°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. United States operates approximately 12,360 active satellites in total, of which 1,167 share a similar altitude band with APEX ARIES 1.
❓ Frequently Asked Questions
APEX ARIES 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 400 km altitude. Its 97.5° 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 93 minutes, travelling at 27,622 km/h.
APEX ARIES 1 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 59129. You can track APEX ARIES 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
APEX ARIES 1 was launched on 2024-03-04 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: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks APEX ARIES 1 (NORAD ID 59129) 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.
APEX ARIES 1 travels at approximately 27,622 km/h (17,164 mph) — roughly 7.67 km/s. It completes 15.56 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.