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 59386U 26145.58206400 +.00000000 +00000-0 +20984-4 0 00004
2 59386 53.1609 260.6668 0001145 71.7733 288.3394 15.34387677 08
| Epoch (UTC): | 25 May 2026 13:58:10 |
| Eccentricity: | 0.0001145 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 260.6668° |
| argument of perigee: | 71.7733° |
| revolutions per day: | 15.34387677 |
| mean anomaly at epoch: | 288.3394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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