PUNCH-WFI01
NORAD 63179
Payload
LEO
2025-047B
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LEO · NORAD 63179
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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
641 km
Apogee
654 km
Inclination
98.0°
Period
97.7 min
Mean Motion
14.74350743 rev/day
TLE Epoch
2026-06-19 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude648 km
Orbital Velocity27,130 km/h
Velocity7.54 km/s
Orbital Period98 minutes
Orbits / Day14.74
Eccentricity0.0009
Semi-Major Axis7,019 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2025-03-12
Launch Site
Vandenberg SFB, California
Int'l Designator
2025-047B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
PUNCH-WFI01 is an active satellite operated by United States, launched on 2025-03-12 from Vandenberg SFB, California. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 641 km and 654 km with an inclination of 98.0°. It travels at approximately 27,130 km/h (7.54 km/s), completing one full orbit every 98 minutes — that’s roughly 14.74 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 PUNCH-WFI01 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
PUNCH-WFI01 orbits at an average altitude of 648 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 PUNCH-WFI01’s average altitude, there are currently 693 active payloads and 1,013 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA. With an inclination of 98.0°, PUNCH-WFI01 passes over latitudes between 98.0°N and 98.0°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 12,339 active satellites in total, of which 298 share a similar altitude band with PUNCH-WFI01.
❓ Frequently Asked Questions
PUNCH-WFI01 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 648 km altitude. Its 98.0° 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 98 minutes, travelling at 27,130 km/h.
PUNCH-WFI01 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 63179. You can track PUNCH-WFI01 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
PUNCH-WFI01 was launched on 2025-03-12 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks PUNCH-WFI01 (NORAD ID 63179) 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.
PUNCH-WFI01 travels at approximately 27,130 km/h (16,858 mph) — roughly 7.54 km/s. It completes 14.74 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.