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 59039U 26145.15962198 +.00000000 +00000-0 +36745-3 0 00006
2 59039 43.0003 315.1214 0001299 276.2575 83.8129 15.27605744 02
| Epoch (UTC): | 25 May 2026 03:49:51 |
| Eccentricity: | 0.0001299 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 315.1214° |
| argument of perigee: | 276.2575° |
| revolutions per day: | 15.27605744 |
| mean anomaly at epoch: | 83.8129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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