LUMELITE 4, 56309
Orbit data source: Space-Track
LUMELITE 4, 56309 is a payload satellite owned by NUS (SG) in LEO that was launched on Sat, 22 Apr 2023 UTC via a PSLV launch vehicle from the Sirharikota (SRI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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56309 intel report (Beta)
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Identifier
Orbit
Country
SG / SINGRelated business
Manufacturer
NUS
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
16 kg wet, 16 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.200 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LUMELITE 4
1 56309U 23057B 26093.69537069 .00020795 00000-0 87831-3 0 9998
2 56309 9.9930 264.2204 0004130 80.9863 279.0821 15.20552987162694Epoch: 2026-04-03T16:41Z
TLE epoch observation values (Epoch: 2026-04-03T16:41:20.027Z)
Latitude
0.00001°
Longitude
-178.13882°
Altitude
500.731 km
Speed
7.618 km/s
True Right ascension
17h 36m 52s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:49:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.135 km
Perigee altitude
507.445 km
Semi-major axis
6,888.427 km
Eccentricity
0.00041
Inclination
9.993°
RAAN
264.2204°
Arg. of periapsis
80.9863°
True anomaly
279.03536°
Mean anomaly
279.0821°
Eccentric anomaly
279.05873°
Mean motion
3.79632 °/min
Orbital period
94.83 mins
BSTAR
0.00087831
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Other satellites on launch #57 in the year 2023 (2023-04-22 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.LUMELITE 4 Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| LUMELITE 4 is likely not visible in the next few days. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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