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 59683U 26145.30260646 +.00000000 +00000-0 +25149-4 0 00004
2 59683 43.0039 351.1289 0001372 260.9138 99.1558 15.27575567 00
| Epoch (UTC): | 25 May 2026 07:15:45 |
| Eccentricity: | 0.0001372 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 351.1289° |
| argument of perigee: | 260.9138° |
| revolutions per day: | 15.27575567 |
| mean anomaly at epoch: | 99.1558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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