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OMNI-M1

NORAD 26857 Payload MEO 2001-026A ● Active
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
10577 km
Apogee
10625 km
Inclination
44.8°
Period
367.0 min
Mean Motion
3.92401638 rev/day
TLE Epoch
2026-06-16 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude10,601 km
Orbital Velocity17,446 km/h
Velocity4.85 km/s
Orbital Period6 hours 7 minutes
Orbits / Day3.92
Eccentricity0.0014
Semi-Major Axis16,972 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
New ICO
Launch Date
2001-06-19
Launch Site
Cape Canaveral, Florida
Int'l Designator
2001-026A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OMNI-M1 is an active satellite operated by New ICO, launched on 2001-06-19 from Cape Canaveral, Florida. With over 25 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 10,577 km and 10,625 km with an inclination of 44.8°. It travels at approximately 17,446 km/h (4.85 km/s), completing one full orbit every 6 hours 7 minutes — that’s roughly 3.92 orbits per day. Orbital Radar tracks OMNI-M1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OMNI-M1 orbits at an average altitude of 10,601 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of OMNI-M1’s average altitude, there are currently 1 active payload and 3 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 44.8°, OMNI-M1 passes over latitudes between 44.8°N and 44.8°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.
❓ Frequently Asked Questions
OMNI-M1 orbits in Medium Earth Orbit (MEO) at altitudes between 10,577 km (perigee) and 10,625 km (apogee), with an average altitude of approximately 10,601 km. It completes one orbit every 6 hours 7 minutes, travelling at approximately 17,446 km/h (10,841 mph).
OMNI-M1 is operated by New ICO. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26857. You can track OMNI-M1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OMNI-M1 was launched on 2001-06-19 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. View the full satellite launch log.
Yes — Orbital Radar tracks OMNI-M1 (NORAD ID 26857) 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.
OMNI-M1 travels at approximately 17,446 km/h (10,841 mph) — roughly 4.85 km/s. It completes 3.92 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 8 sunrises and sunsets every 24 hours.