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 65598U 26145.44885830 +.00000000 +00000-0 +24682-3 0 00009
2 65598 97.4504 213.9825 0002469 143.7327 216.4068 15.05653205 01
| Epoch (UTC): | 25 May 2026 10:46:21 |
| Eccentricity: | 0.0002469 |
| inclination: | 97.4504° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.9825° |
| argument of perigee: | 143.7327° |
| revolutions per day: | 15.05653205 |
| mean anomaly at epoch: | 216.4068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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