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 65352U 26145.36005912 +.00000000 +00000-0 +39047-3 0 00004
2 65352 53.1573 172.0644 0000870 79.2432 280.8667 15.30206042 03
| Epoch (UTC): | 25 May 2026 08:38:29 |
| Eccentricity: | 0.0000870 |
| inclination: | 53.1573° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 172.0644° |
| argument of perigee: | 79.2432° |
| revolutions per day: | 15.30206042 |
| mean anomaly at epoch: | 280.8667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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