OBJECT A
NORAD 100125
Unknown
HEO
2026-167A
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HEO · NORAD 100125
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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
1244 km
Apogee
47037 km
Inclination
23.3°
Period
884.3 min
Mean Motion
1.62838602 rev/day
TLE Epoch
2026-09-17 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude24,141 km
Orbital Velocity13,012 km/h
Velocity3.61 km/s
Orbital Period14 hours 44 minutes
Orbits / Day1.63
Eccentricity0.7504
Semi-Major Axis30,512 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2026-07-21
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
2026-167A
Object Type
Unknown
RCS Size
Unknown
📖 About This Object
OBJECT A (NORAD ID 100125) is a space object catalogued under United States, launched on 2026-07-21 from Cape Canaveral Space Force Station, United States on the MRV/MEP launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 1,244 km and 47,037 km with an inclination of 23.3°. It travels at approximately 13,012 km/h (3.61 km/s), completing one full orbit every 14 hours 44 minutes — that’s roughly 1.63 orbits per day. Its orbital eccentricity of 0.7504 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks OBJECT A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OBJECT A follows a Highly Elliptical Orbit, sweeping between 1,244 km (perigee) and 47,037 km (apogee). It spends most of its 14 hours 44 minutes 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. With an inclination of 23.3°, OBJECT A passes over latitudes between 23.3°N and 23.3°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 13,196 active satellites in total.
❓ Frequently Asked Questions
OBJECT A follows a Highly Elliptical Orbit, swinging between 1,244 km (perigee) and 47,037 km (apogee). It spends most of its 14 hours 44 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
OBJECT A was launched on 2026-07-21 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT A (NORAD ID 100125) 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.
OBJECT A’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 13,012 km/h (3.61 km/s), completing one revolution every 14 hours 44 minutes. Learn more about highly elliptical orbits.