LVM3 R/B, 66310
Orbit data source: Space-Track
LVM3 R/B, 66310 is space debris in HEO originally from a launch on Sun, 02 Nov 2025 UTC launched from the Sirharikota (SRI). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Spacecraft
Bus & Motor
C25, CE-20
Mass
4,400 kg wet, 4,400 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 8.0 m
Radar Cross Section
48.836 m²
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 LVM3 R/B
1 66310U 25249A 26061.30680671 .00188524 11906-6 52203-3 0 9990
2 66310 21.3834 89.3249 6586342 305.7519 9.4510 3.29051996 3835Epoch: 2026-03-02T07:21Z
TLE epoch observation values (Epoch: 2026-03-02T07:21:48.099Z)
Latitude
0.00021°
Longitude
178.84663°
Altitude
1,442.6 km
Speed
9.003 km/s
True Right ascension
05h 57m 35s
True Declination
0° 00' 01"
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
07:01:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
25,298.687 km
Perigee altitude
141.314 km
Semi-major axis
19,098.137 km
Eccentricity
0.65863
Inclination
21.3834°
RAAN
89.3249°
Arg. of periapsis
305.7519°
True anomaly
53.91471°
Mean anomaly
9.451°
Eccentric anomaly
25.98479°
Mean motion
0.82235 °/min
Orbital period
437.77 mins
BSTAR
0.00052203
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Other satellites on launch #249 in the year 2025 (2025-11-02 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.LVM3 R/B Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 366 mins | 2026-03-03 05:21:32.659Z | 221.95° SW | 2026-03-03 05:54:32.659Z | 147.236° SSE | 39.222° | 2026-03-03 11:27:32.659Z | 124.388° SE |
| 8 mins | 2026-03-04 03:10:32.659Z | 174.566° S | 2026-03-04 03:18:32.659Z | 143.396° SSE | 24.872° | 2026-03-04 03:18:32.659Z | 143.396° SSE |
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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