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 57102U 26145.53101123 +.00000000 +00000-0 +22028-4 0 00000
2 57102 43.0038 207.6507 0001302 269.6807 90.3895 15.26744385 05
| Epoch (UTC): | 25 May 2026 12:44:39 |
| Eccentricity: | 0.0001302 |
| inclination: | 43.0038° |
| perigee height: | 485 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 207.6507° |
| argument of perigee: | 269.6807° |
| revolutions per day: | 15.26744385 |
| mean anomaly at epoch: | 90.3895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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