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 68825U 26145.29225968 +.00000000 +00000-0 +20337-2 0 00000
2 68825 97.2850 351.9773 0002083 72.9265 287.2228 15.75263715 04
| Epoch (UTC): | 25 May 2026 07:00:51 |
| Eccentricity: | 0.0002083 |
| inclination: | 97.2850° |
| perigee height: | 342 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 351.9773° |
| argument of perigee: | 72.9265° |
| revolutions per day: | 15.75263715 |
| mean anomaly at epoch: | 287.2228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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