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HAMMER

NORAD 59148 Payload LEO 2024-043BC ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
393 km
Apogee
397 km
Inclination
97.5°
Period
92.5 min
Mean Motion
15.57527779 rev/day
TLE Epoch
2026-09-17 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude395 km
Orbital Velocity27,632 km/h
Velocity7.68 km/s
Orbital Period92 minutes
Orbits / Day15.58
Eccentricity0.0003
Semi-Major Axis6,766 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇪🇸 Open Cosmos (Spain)
Launch Date
2024-03-04
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2024-043BC
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
HAMMER is an active satellite operated by Open Cosmos (Spain), launched on 2024-03-04 from Vandenberg Space Force Base, United States on the Transporter-10 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 393 km and 397 km with an inclination of 97.5°. It travels at approximately 27,632 km/h (7.68 km/s), completing one full orbit every 92 minutes — that’s roughly 15.58 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 HAMMER in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
HAMMER orbits at an average altitude of 395 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 HAMMER’s average altitude, there are currently 1,247 active payloads and 83 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1008, STARLINK-1012. This makes it one of the more crowded altitude bands, containing roughly 6.7% of all active satellites. With an inclination of 97.5°, HAMMER 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. Spain operates approximately 56 active satellites in total, of which 8 share a similar altitude band with HAMMER.
❓ Frequently Asked Questions
HAMMER is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 395 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 92 minutes, travelling at 27,632 km/h.
HAMMER is operated by Open Cosmos (Spain). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 59148. You can track HAMMER in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
HAMMER was launched on 2024-03-04 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: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks HAMMER (NORAD ID 59148) 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.
HAMMER travels at approximately 27,632 km/h (17,169 mph) — roughly 7.68 km/s. It completes 15.58 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.