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 59430U 26145.37720788 +.00000000 +00000-0 +27747-4 0 00005
2 59430 53.1614 285.2508 0000730 108.5172 251.5908 15.30178857 02
| Epoch (UTC): | 25 May 2026 09:03:10 |
| Eccentricity: | 0.0000730 |
| inclination: | 53.1614° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 285.2508° |
| argument of perigee: | 108.5172° |
| revolutions per day: | 15.30178857 |
| mean anomaly at epoch: | 251.5908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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