CYGFM05
NORAD 41884
Payload
LEO
2016-078A
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LEO · NORAD 41884
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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
382 km
Apogee
390 km
Inclination
35.0°
Period
92.3 min
Mean Motion
15.60717627 rev/day
TLE Epoch
2026-09-17 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude386 km
Orbital Velocity27,650 km/h
Velocity7.68 km/s
Orbital Period92 minutes
Orbits / Day15.61
Eccentricity0.0006
Semi-Major Axis6,757 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇺🇸 University of Michigan/NASA Earth Science Technology Office (United States)
Launch Date
2016-12-15
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
2016-078A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CYGFM05 is an active satellite operated by University of Michigan/NASA Earth Science Technology Office (United States), launched on 2016-12-15 from Cape Canaveral Space Force Station, United States on the CYGNSS launch. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 382 km and 390 km with an inclination of 35.0°. It travels at approximately 27,650 km/h (7.68 km/s), completing one full orbit every 92 minutes — that’s roughly 15.61 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Orbital Radar tracks CYGFM05 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CYGFM05 orbits at an average altitude of 386 km in the lower reaches of Low Earth Orbit, where atmospheric drag is significant and orbital lifetimes are measured in months to a few years. This is the busiest corridor in space — home to crewed spacecraft, rapid-revisit imaging satellites and the densest part of the Starlink constellation. Within ±50 km of CYGFM05’s average altitude, there are currently 1,347 active payloads and 72 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1008, STARLINK-1012. This makes it one of the more crowded altitude bands, containing roughly 7.2% of all active satellites. With an inclination of 35.0°, CYGFM05 passes over latitudes between 35.0°N and 35.0°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. United States operates approximately 13,204 active satellites in total, of which 1,201 share a similar altitude band with CYGFM05.
❓ Frequently Asked Questions
CYGFM05 orbits in Low Earth Orbit (LEO) at altitudes between 382 km (perigee) and 390 km (apogee), with an average altitude of approximately 386 km. It completes one orbit every 92 minutes, travelling at approximately 27,650 km/h (17,181 mph).
CYGFM05 is operated by University of Michigan/NASA Earth Science Technology Office (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 41884. You can track CYGFM05 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CYGFM05 was launched on 2016-12-15 from Cape Canaveral Space Force Station, United States, 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: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks CYGFM05 (NORAD ID 41884) 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.
CYGFM05 travels at approximately 27,650 km/h (17,181 mph) — roughly 7.68 km/s. It completes 15.61 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.