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OBJECT A

NORAD 100125 Payload HEO 2026-167A ● Active
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
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🛰️ Orbital Parameters
Perigee
3351 km
Apogee
51468 km
Inclination
19.3°
Period
1030.1 min
Mean Motion
1.39786924 rev/day
TLE Epoch
2026-11-01 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude27,410 km
Orbital Velocity12,366 km/h
Velocity3.44 km/s
Orbital Period17 hours 10 minutes
Orbits / Day1.40
Eccentricity0.7122
Semi-Major Axis33,781 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 Space Logistics (United States)
Launch Date
2026-07-21
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
2026-167A
Object Type
Payload
RCS Size
Unknown
📖 About This Object
OBJECT A is an active satellite operated by Space Logistics (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 3,351 km and 51,468 km with an inclination of 19.3°. It travels at approximately 12,366 km/h (3.44 km/s), completing one full orbit every 17 hours 10 minutes — that’s roughly 1.40 orbits per day. Its orbital eccentricity of 0.7122 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 3,351 km (perigee) and 51,468 km (apogee). It spends most of its 17 hours 10 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 19.3°, OBJECT A passes over latitudes between 19.3°N and 19.3°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. United States operates approximately 13,350 active satellites in total.
❓ Frequently Asked Questions
OBJECT A follows a Highly Elliptical Orbit, swinging between 3,351 km (perigee) and 51,468 km (apogee). It spends most of its 17 hours 10 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
OBJECT A is operated by Space Logistics (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 100125. You can track OBJECT A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
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. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT A (NORAD ID 100125) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 12,366 km/h (3.44 km/s), completing one revolution every 17 hours 10 minutes. Learn more about highly elliptical orbits.