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 42803U 26145.49582573 +.00000000 +00000-0 +10031-4 0 00000
2 42803 86.3962 331.6681 0002326 91.7409 268.4054 14.34217551 06
| Epoch (UTC): | 25 May 2026 11:53:59 |
| Eccentricity: | 0.0002326 |
| inclination: | 86.3962° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 331.6681° |
| argument of perigee: | 91.7409° |
| revolutions per day: | 14.34217551 |
| mean anomaly at epoch: | 268.4054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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