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 68745U 26145.58335647 +.00000000 +00000-0 -56977-1 0 00008
2 68745 97.2849 9.2355 0001796 107.6423 228.9416 15.51673815 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001796 |
| inclination: | 97.2849° |
| perigee height: | 411 km |
| apogee height: | 413 km |
| right ascension of ascending node: | 9.2355° |
| argument of perigee: | 107.6423° |
| revolutions per day: | 15.51673815 |
| mean anomaly at epoch: | 228.9416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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