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MMS 4

NORAD 40485 Payload HEO 2015-011D ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
10041 km
Apogee
172971 km
Inclination
72.2°
Period
5079.6 min
Mean Motion
0.28346385 rev/day
TLE Epoch
2026-06-19 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude91,506 km
Orbital Velocity7,265 km/h
Velocity2.02 km/s
Orbital Period84.7 hours
Orbits / Day0.28
Eccentricity0.8323
Semi-Major Axis97,877 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 National Aeronautics and Space Administration (NASA) (United States)
Launch Date
2015-03-13
Launch Site
Cape Canaveral, Florida
Int'l Designator
2015-011D
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MMS 4 is an active satellite operated by National Aeronautics and Space Administration (NASA) (United States), launched on 2015-03-13 from Cape Canaveral, Florida. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 10,041 km and 172,971 km with an inclination of 72.2°. It travels at approximately 7,265 km/h (2.02 km/s), completing one full orbit every 84.7 hours — that’s roughly 0.28 orbits per day. Its orbital eccentricity of 0.8323 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks MMS 4 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
MMS 4 follows a Highly Elliptical Orbit, sweeping between 10,041 km (perigee) and 172,971 km (apogee). It spends most of its 84.7 hours orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. Within ±50 km of MMS 4’s average altitude, there are currently 4 active payloads and 0 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 72.2°, MMS 4 passes over latitudes between 72.2°N and 72.2°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 12,339 active satellites in total, of which 4 share a similar altitude band with MMS 4.
❓ Frequently Asked Questions
MMS 4 follows a Highly Elliptical Orbit, swinging between 10,041 km (perigee) and 172,971 km (apogee). It spends most of its 84.7 hours orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
MMS 4 is operated by National Aeronautics and Space Administration (NASA) (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 40485. You can track MMS 4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MMS 4 was launched on 2015-03-13 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 MMS 4 (NORAD ID 40485) 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.
MMS 4’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 7,265 km/h (2.02 km/s), completing one revolution every 84.7 hours. Learn more about highly elliptical orbits.