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 68768U 26145.58335647 +.00000000 +00000-0 -26097-1 0 00003
2 68768 97.2848 182.4207 0001473 76.3825 17.5802 15.60031447 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001473 |
| inclination: | 97.2848° |
| perigee height: | 387 km |
| apogee height: | 389 km |
| right ascension of ascending node: | 182.4207° |
| argument of perigee: | 76.3825° |
| revolutions per day: | 15.60031447 |
| mean anomaly at epoch: | 17.5802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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