SEMI-1P
NORAD 66298
Payload
LEO
2025-248F
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LEO · NORAD 66298
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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
494 km
Apogee
511 km
Inclination
45.4°
Period
94.7 min
Mean Motion
15.21042385 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude503 km
Orbital Velocity27,415 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.21
Eccentricity0.0012
Semi-Major Axis6,874 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
Turkey
Launch Date
2025-11-02
Launch Site
Cape Canaveral, Florida
Int'l Designator
2025-248F
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SEMI-1P is an active satellite operated by Turkey, launched on 2025-11-02 from Cape Canaveral, Florida. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 494 km and 511 km with an inclination of 45.4°. It travels at approximately 27,415 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.21 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks SEMI-1P in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SEMI-1P orbits at an average altitude of 503 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of SEMI-1P’s average altitude, there are currently 9,586 active payloads and 248 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 55% of all active satellites. With an inclination of 45.4°, SEMI-1P passes over latitudes between 45.4°N and 45.4°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. Turkey operates approximately 41 active satellites in total, of which 19 share a similar altitude band with SEMI-1P.
❓ Frequently Asked Questions
SEMI-1P orbits in Low Earth Orbit (LEO) at altitudes between 494 km (perigee) and 511 km (apogee), with an average altitude of approximately 503 km. It completes one orbit every 95 minutes, travelling at approximately 27,415 km/h (17,035 mph).
SEMI-1P is operated by Turkey. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 66298. You can track SEMI-1P in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SEMI-1P was launched on 2025-11-02 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks SEMI-1P (NORAD ID 66298) 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.
SEMI-1P travels at approximately 27,415 km/h (17,035 mph) — roughly 7.62 km/s. It completes 15.21 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.