ASTRANIS UTILITYSAT
NORAD 62454
Payload
HEO
2024-252A
● Active
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HEO · NORAD 62454
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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
3909 km
Apogee
67642 km
Inclination
9.1°
Period
1435.5 min
Mean Motion
1.00311838 rev/day
TLE Epoch
2026-10-22 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,776 km
Orbital Velocity11,071 km/h
Velocity3.08 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.7561
Semi-Major Axis42,147 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇬🇧 Spacing Guild UK (United Kingdom)
Launch Date
2024-12-29
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
2024-252A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ASTRANIS UTILITYSAT is an active satellite operated by Spacing Guild UK (United Kingdom), launched on 2024-12-29 from Cape Canaveral Space Force Station, United States on the Astranis launch. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 3,909 km and 67,642 km with an inclination of 9.1°. It travels at approximately 11,071 km/h (3.08 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. Its orbital eccentricity of 0.7561 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 ASTRANIS UTILITYSAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ASTRANIS UTILITYSAT follows a Highly Elliptical Orbit, sweeping between 3,909 km (perigee) and 67,642 km (apogee). It spends most of its ~24 hours (geosynchronous) 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 ASTRANIS UTILITYSAT’s average altitude, there are currently 739 active payloads and 61 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. With an inclination of 9.1°, ASTRANIS UTILITYSAT passes over latitudes between 9.1°N and 9.1°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. United Kingdom operates approximately 725 active satellites in total, of which 13 share a similar altitude band with ASTRANIS UTILITYSAT.
❓ Frequently Asked Questions
ASTRANIS UTILITYSAT follows a Highly Elliptical Orbit, swinging between 3,909 km (perigee) and 67,642 km (apogee). It spends most of its ~24 hours (geosynchronous) orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
ASTRANIS UTILITYSAT is operated by Spacing Guild UK (United Kingdom). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 62454. You can track ASTRANIS UTILITYSAT in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ASTRANIS UTILITYSAT was launched on 2024-12-29 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 ASTRANIS UTILITYSAT (NORAD ID 62454) 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.
ASTRANIS UTILITYSAT’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 11,071 km/h (3.08 km/s), completing one revolution every ~24 hours (geosynchronous). Learn more about highly elliptical orbits.