TANSEI 1 (MS-T1)
NORAD 4952
Payload
LEO
1971-011A
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🛰️ Orbital Parameters
Perigee
981 km
Apogee
1100 km
Inclination
29.7°
Period
106.0 min
Mean Motion
13.58643879 rev/day
TLE Epoch
2026-10-21 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,041 km
Orbital Velocity26,401 km/h
Velocity7.33 km/s
Orbital Period106 minutes
Orbits / Day13.59
Eccentricity0.0080
Semi-Major Axis7,412 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇯🇵 ISAS (Japan)
Launch Date
1971-02-16
Launch Site
Uchinoura Space Center, Japan
Int'l Designator
1971-011A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
TANSEI 1 (MS-T1) is an active satellite operated by ISAS (Japan), launched on 1971-02-16 from Uchinoura Space Center, Japan on the MS-T1 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 981 km and 1,100 km with an inclination of 29.7°. It travels at approximately 26,401 km/h (7.33 km/s), completing one full orbit every 106 minutes — that’s roughly 13.59 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Orbital Radar tracks TANSEI 1 (MS-T1) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TANSEI 1 (MS-T1) orbits at an average altitude of 1,041 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of TANSEI 1 (MS-T1)’s average altitude, there are currently 322 active payloads and 681 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 29.7°, TANSEI 1 (MS-T1) passes over latitudes between 29.7°N and 29.7°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 7 share a similar altitude band with TANSEI 1 (MS-T1).
❓ Frequently Asked Questions
TANSEI 1 (MS-T1) orbits in Low Earth Orbit (LEO) at altitudes between 981 km (perigee) and 1,100 km (apogee), with an average altitude of approximately 1,041 km. It completes one orbit every 106 minutes, travelling at approximately 26,401 km/h (16,405 mph).
TANSEI 1 (MS-T1) is operated by ISAS (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 4952. You can track TANSEI 1 (MS-T1) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TANSEI 1 (MS-T1) was launched on 1971-02-16 from Uchinoura Space Center, Japan. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks TANSEI 1 (MS-T1) (NORAD ID 4952) 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.
TANSEI 1 (MS-T1) travels at approximately 26,401 km/h (16,405 mph) — roughly 7.33 km/s. It completes 13.59 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.