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 68617U 26145.58335647 +.00000000 +00000-0 +71926-3 0 00008
2 68617 97.2848 345.1038 0001688 91.4683 76.1225 15.49169477 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001688 |
| inclination: | 97.2848° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 345.1038° |
| argument of perigee: | 91.4683° |
| revolutions per day: | 15.49169477 |
| mean anomaly at epoch: | 76.1225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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