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 68621U 26145.58335647 +.00000000 +00000-0 -60491-1 0 00007
2 68621 97.2850 345.0030 0001908 84.6308 203.9548 15.51765224 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001908 |
| inclination: | 97.2850° |
| perigee height: | 410 km |
| apogee height: | 413 km |
| right ascension of ascending node: | 345.0030° |
| argument of perigee: | 84.6308° |
| revolutions per day: | 15.51765224 |
| mean anomaly at epoch: | 203.9548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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