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 57636U 26145.00023874 +.00000000 +00000-0 +10188-3 0 00003
2 57636 43.0018 21.8862 0001517 272.9773 87.0905 15.27592972 01
| Epoch (UTC): | 25 May 2026 00:00:20 |
| Eccentricity: | 0.0001517 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.8862° |
| argument of perigee: | 272.9773° |
| revolutions per day: | 15.27592972 |
| mean anomaly at epoch: | 87.0905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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