CROCUBE
NORAD 62394
Payload
LEO
2024-247T
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LEO · NORAD 62394
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Altitude (km)
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Speed (km/s)
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Longitude
🛰️ Orbital Parameters
Perigee
416 km
Apogee
427 km
Inclination
45.0°
Period
93.0 min
Mean Motion
15.48292245 rev/day
TLE Epoch
2026-06-17 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude422 km
Orbital Velocity27,578 km/h
Velocity7.66 km/s
Orbital Period93 minutes
Orbits / Day15.48
Eccentricity0.0008
Semi-Major Axis6,793 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
HRV
Launch Date
2024-12-21
Launch Site
Vandenberg SFB, California
Int'l Designator
2024-247T
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CROCUBE is an active satellite operated by HRV, launched on 2024-12-21 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 416 km and 427 km with an inclination of 45.0°. It travels at approximately 27,578 km/h (7.66 km/s), completing one full orbit every 93 minutes — that’s roughly 15.48 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Orbital Radar tracks CROCUBE in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CROCUBE orbits at an average altitude of 422 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of CROCUBE’s average altitude, there are currently 3,309 active payloads and 129 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 19% of all active satellites. With an inclination of 45.0°, CROCUBE passes over latitudes between 45.0°N and 45.0°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.
❓ Frequently Asked Questions
CROCUBE orbits in Low Earth Orbit (LEO) at altitudes between 416 km (perigee) and 427 km (apogee), with an average altitude of approximately 422 km. It completes one orbit every 93 minutes, travelling at approximately 27,578 km/h (17,136 mph).
CROCUBE is operated by HRV. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 62394. You can track CROCUBE in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CROCUBE was launched on 2024-12-21 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks CROCUBE (NORAD ID 62394) 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.
CROCUBE travels at approximately 27,578 km/h (17,136 mph) — roughly 7.66 km/s. It completes 15.48 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.