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 68607U 26145.58335647 +.00000000 +00000-0 -35195-1 0 00004
2 68607 97.2841 345.0260 0001158 72.9080 279.7433 15.55189235 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001158 |
| inclination: | 97.2841° |
| perigee height: | 401 km |
| apogee height: | 402 km |
| right ascension of ascending node: | 345.0260° |
| argument of perigee: | 72.9080° |
| revolutions per day: | 15.55189235 |
| mean anomaly at epoch: | 279.7433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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