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 68826U 26145.50136523 +.00000000 +00000-0 +17146-3 0 00008
2 68826 96.6466 63.9917 0018326 119.8736 240.4359 15.81261782 07
| Epoch (UTC): | 25 May 2026 12:01:57 |
| Eccentricity: | 0.0018326 |
| inclination: | 96.6466° |
| perigee height: | 315 km |
| apogee height: | 339 km |
| right ascension of ascending node: | 63.9917° |
| argument of perigee: | 119.8736° |
| revolutions per day: | 15.81261782 |
| mean anomaly at epoch: | 240.4359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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