LUMELITE 4
NORAD 56309
Payload
LEO
2023-057B
● Active
CONNECTING…
LEO · NORAD 56309
NOW PASSING OVER
Calculating position…
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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
497 km
Apogee
502 km
Inclination
10.0°
Period
94.6 min
Mean Motion
15.22044216 rev/day
TLE Epoch
2026-06-19 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude500 km
Orbital Velocity27,421 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.22
Eccentricity0.0004
Semi-Major Axis6,871 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
Singapore
Launch Date
2023-04-22
Launch Site
SRI
Int'l Designator
2023-057B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LUMELITE 4 is an active satellite operated by Singapore, launched on 2023-04-22 from SRI. It orbits in Low Earth Orbit (LEO) at altitudes between 497 km and 502 km with an inclination of 10.0°. It travels at approximately 27,421 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.22 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 LUMELITE 4 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
LUMELITE 4 orbits at an average altitude of 500 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 LUMELITE 4’s average altitude, there are currently 9,617 active payloads and 241 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 55.2% of all active satellites. With an inclination of 10.0°, LUMELITE 4 passes over latitudes between 10.0°N and 10.0°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. Singapore operates approximately 14 active satellites in total, of which 5 share a similar altitude band with LUMELITE 4.
❓ Frequently Asked Questions
LUMELITE 4 orbits in Low Earth Orbit (LEO) at altitudes between 497 km (perigee) and 502 km (apogee), with an average altitude of approximately 500 km. It completes one orbit every 95 minutes, travelling at approximately 27,421 km/h (17,038 mph).
LUMELITE 4 is operated by Singapore. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 56309. You can track LUMELITE 4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
LUMELITE 4 was launched on 2023-04-22 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks LUMELITE 4 (NORAD ID 56309) 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.
LUMELITE 4 travels at approximately 27,421 km/h (17,038 mph) — roughly 7.62 km/s. It completes 15.22 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.