SHINSEI (MS-F2)
NORAD 5485
Payload
LEO
1971-080A
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🛰️ Orbital Parameters
Perigee
869 km
Apogee
1860 km
Inclination
32.0°
Period
113.0 min
Mean Motion
12.74258455 rev/day
TLE Epoch
2026-10-21 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,365 km
Orbital Velocity25,842 km/h
Velocity7.18 km/s
Orbital Period113 minutes
Orbits / Day12.74
Eccentricity0.0641
Semi-Major Axis7,736 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇯🇵 ISAS (Japan)
Launch Date
1971-09-28
Launch Site
Uchinoura Space Center, Japan
Int'l Designator
1971-080A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SHINSEI (MS-F2) is an active satellite operated by ISAS (Japan), launched on 1971-09-28 from Uchinoura Space Center, Japan on the MS-F2 launch. After more than 55 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 869 km and 1,860 km with an inclination of 32.0°. It travels at approximately 25,842 km/h (7.18 km/s), completing one full orbit every 113 minutes — that’s roughly 12.74 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Orbital Radar tracks SHINSEI (MS-F2) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SHINSEI (MS-F2) orbits at an average altitude of 1,365 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of SHINSEI (MS-F2)’s average altitude, there are currently 184 active payloads and 254 tracked debris or rocket body fragments. With an inclination of 32.0°, SHINSEI (MS-F2) passes over latitudes between 32.0°N and 32.0°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. Japan operates approximately 209 active satellites in total, of which 3 share a similar altitude band with SHINSEI (MS-F2).
❓ Frequently Asked Questions
SHINSEI (MS-F2) orbits in Low Earth Orbit (LEO) at altitudes between 869 km (perigee) and 1,860 km (apogee), with an average altitude of approximately 1,365 km. It completes one orbit every 113 minutes, travelling at approximately 25,842 km/h (16,058 mph).
SHINSEI (MS-F2) is operated by ISAS (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 5485. You can track SHINSEI (MS-F2) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SHINSEI (MS-F2) was launched on 1971-09-28 from Uchinoura Space Center, Japan. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks SHINSEI (MS-F2) (NORAD ID 5485) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
SHINSEI (MS-F2) travels at approximately 25,842 km/h (16,058 mph) — roughly 7.18 km/s. It completes 12.74 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.