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 58505U 26145.61884611 +.00000000 +00000-0 +71949-4 0 00003
2 58505 86.5033 340.3933 0002027 100.2200 259.9172 13.39550458 09
| Epoch (UTC): | 25 May 2026 14:51:08 |
| Eccentricity: | 0.0002027 |
| inclination: | 86.5033° |
| perigee height: | 1109 km |
| apogee height: | 1112 km |
| right ascension of ascending node: | 340.3933° |
| argument of perigee: | 100.2200° |
| revolutions per day: | 13.39550458 |
| mean anomaly at epoch: | 259.9172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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