SEDNA-2
NORAD 63153
Payload
LEO
2025-009DQ
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LEO · NORAD 63153
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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
520 km
Apogee
534 km
Inclination
97.5°
Period
95.2 min
Mean Motion
15.12944773 rev/day
TLE Epoch
2026-09-17 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude527 km
Orbital Velocity27,366 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.13
Eccentricity0.0010
Semi-Major Axis6,898 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 CLAAC (United States)
Launch Date
2025-01-14
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2025-009DQ
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SEDNA-2 is an active satellite operated by CLAAC (United States), launched on 2025-01-14 from Vandenberg Space Force Base, United States on the Transporter-12 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 520 km and 534 km with an inclination of 97.5°. It travels at approximately 27,366 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.13 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks SEDNA-2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SEDNA-2 orbits at an average altitude of 527 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 SEDNA-2’s average altitude, there are currently 5,212 active payloads and 304 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 27.9% of all active satellites. With an inclination of 97.5°, SEDNA-2 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 13,204 active satellites in total, of which 4,525 share a similar altitude band with SEDNA-2.
❓ Frequently Asked Questions
SEDNA-2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 527 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 95 minutes, travelling at 27,366 km/h.
SEDNA-2 is operated by CLAAC (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 63153. You can track SEDNA-2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SEDNA-2 was launched on 2025-01-14 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks SEDNA-2 (NORAD ID 63153) 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.
SEDNA-2 travels at approximately 27,366 km/h (17,004 mph) — roughly 7.60 km/s. It completes 15.13 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.