ASBM-1
NORAD 60422
Payload
HEO
2024-143A
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HEO · NORAD 60422
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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
7585 km
Apogee
44009 km
Inclination
63.0°
Period
957.3 min
Mean Motion
1.50423653 rev/day
TLE Epoch
2026-10-27 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude25,797 km
Orbital Velocity12,672 km/h
Velocity3.52 km/s
Orbital Period15 hours 57 minutes
Orbits / Day1.50
Eccentricity0.5662
Semi-Major Axis32,168 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇳🇴 Space Norway / USSF SSC (Norway)
Launch Date
2024-08-12
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2024-143A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ASBM-1 is an active satellite operated by Space Norway / USSF SSC (Norway), launched on 2024-08-12 from Vandenberg Space Force Base, United States on the ASBM-1/2 launch. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 7,585 km and 44,009 km with an inclination of 63.0°. It travels at approximately 12,672 km/h (3.52 km/s), completing one full orbit every 15 hours 57 minutes — that’s roughly 1.50 orbits per day. Its orbital eccentricity of 0.5662 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks ASBM-1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ASBM-1 follows a Highly Elliptical Orbit, sweeping between 7,585 km (perigee) and 44,009 km (apogee). It spends most of its 15 hours 57 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. Within ±50 km of ASBM-1’s average altitude, there are currently 2 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 63.0°, ASBM-1 passes over latitudes between 63.0°N and 63.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Norway operates approximately 27 active satellites in total, of which 2 share a similar altitude band with ASBM-1.
❓ Frequently Asked Questions
ASBM-1 follows a Highly Elliptical Orbit, swinging between 7,585 km (perigee) and 44,009 km (apogee). It spends most of its 15 hours 57 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
ASBM-1 is operated by Space Norway / USSF SSC (Norway). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 60422. You can track ASBM-1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ASBM-1 was launched on 2024-08-12 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. View the full satellite launch log.
Yes — Orbital Radar tracks ASBM-1 (NORAD ID 60422) 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.
ASBM-1’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 12,672 km/h (3.52 km/s), completing one revolution every 15 hours 57 minutes. Learn more about highly elliptical orbits.