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 68823U 26145.29437271 +.00000000 +00000-0 +13716-2 0 00003
2 68823 97.2842 351.9749 0001645 76.2486 283.8962 15.75258794 09
| Epoch (UTC): | 25 May 2026 07:03:53 |
| Eccentricity: | 0.0001645 |
| inclination: | 97.2842° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 351.9749° |
| argument of perigee: | 76.2486° |
| revolutions per day: | 15.75258794 |
| mean anomaly at epoch: | 283.8962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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