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 59071U 26145.61536558 +.00000000 +00000-0 +32079-3 0 00006
2 59071 95.3921 219.7926 0145849 46.7786 314.5510 14.93593291 03
| Epoch (UTC): | 25 May 2026 14:46:07 |
| Eccentricity: | 0.0145849 |
| inclination: | 95.3921° |
| perigee height: | 485 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 219.7926° |
| argument of perigee: | 46.7786° |
| revolutions per day: | 14.93593291 |
| mean anomaly at epoch: | 314.5510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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