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 68350U 26145.38683104 +.00000000 +00000-0 +76591-4 0 00008
2 68350 54.9795 129.1423 0010637 57.9923 302.2108 14.72821798 02
| Epoch (UTC): | 25 May 2026 09:17:02 |
| Eccentricity: | 0.0010637 |
| inclination: | 54.9795° |
| perigee height: | 645 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 129.1423° |
| argument of perigee: | 57.9923° |
| revolutions per day: | 14.72821798 |
| mean anomaly at epoch: | 302.2108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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