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 68822U 26145.04097399 +.00000000 +00000-0 +22962-2 0 00001
2 68822 97.2848 351.7075 0002337 43.2009 316.9439 15.75487449 06
| Epoch (UTC): | 25 May 2026 00:59:00 |
| Eccentricity: | 0.0002337 |
| inclination: | 97.2848° |
| perigee height: | 342 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 351.7075° |
| argument of perigee: | 43.2009° |
| revolutions per day: | 15.75487449 |
| mean anomaly at epoch: | 316.9439° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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