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 68603U 26145.58335647 +.00000000 +00000-0 +36750-3 0 00009
2 68603 97.2846 345.0194 0001279 71.3524 260.7578 15.49175885 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001279 |
| inclination: | 97.2846° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 345.0194° |
| argument of perigee: | 71.3524° |
| revolutions per day: | 15.49175885 |
| mean anomaly at epoch: | 260.7578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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