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 59457U 26145.51692593 +.00000000 +00000-0 +18482-3 0 00007
2 59457 42.9987 317.0833 0000802 280.3797 79.6965 15.27583991 04
| Epoch (UTC): | 25 May 2026 12:24:22 |
| Eccentricity: | 0.0000802 |
| inclination: | 42.9987° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.0833° |
| argument of perigee: | 280.3797° |
| revolutions per day: | 15.27583991 |
| mean anomaly at epoch: | 79.6965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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