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 68608U 26145.50003470 +.00000000 +00000-0 -50320-1 0 00000
2 68608 97.2845 345.0974 0002059 107.5593 140.0101 15.53379356 07
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0002059 |
| inclination: | 97.2845° |
| perigee height: | 405 km |
| apogee height: | 408 km |
| right ascension of ascending node: | 345.0974° |
| argument of perigee: | 107.5593° |
| revolutions per day: | 15.53379356 |
| mean anomaly at epoch: | 140.0101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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