View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65460U 26145.34464144 +.00000000 +00000-0 +95848-3 0 00009
2 65460 53.1594 261.8646 0001383 70.5263 289.5889 15.34406726 08
| Epoch (UTC): | 25 May 2026 08:16:17 |
| Eccentricity: | 0.0001383 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 261.8646° |
| argument of perigee: | 70.5263° |
| revolutions per day: | 15.34406726 |
| mean anomaly at epoch: | 289.5889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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