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 65360U 26145.46269264 +.00000000 +00000-0 +44972-3 0 00009
2 65360 53.1590 171.2855 0001016 60.2133 299.8971 15.34410316 00
| Epoch (UTC): | 25 May 2026 11:06:16 |
| Eccentricity: | 0.0001016 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 171.2855° |
| argument of perigee: | 60.2133° |
| revolutions per day: | 15.34410316 |
| mean anomaly at epoch: | 299.8971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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