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 58685U 26145.35361057 +.00000000 +00000-0 +22864-4 0 00009
2 58685 43.0048 11.9498 0001308 264.6968 95.3734 15.27577806 07
| Epoch (UTC): | 25 May 2026 08:29:11 |
| Eccentricity: | 0.0001308 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 11.9498° |
| argument of perigee: | 264.6968° |
| revolutions per day: | 15.27577806 |
| mean anomaly at epoch: | 95.3734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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