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 68625U 26145.58335647 +.00000000 +00000-0 -34564-1 0 00003
2 68625 97.2847 345.1488 0001597 79.7990 196.9838 15.54591901 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001597 |
| inclination: | 97.2847° |
| perigee height: | 402 km |
| apogee height: | 404 km |
| right ascension of ascending node: | 345.1488° |
| argument of perigee: | 79.7990° |
| revolutions per day: | 15.54591901 |
| mean anomaly at epoch: | 196.9838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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