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 58069U 26145.46955635 +.00000000 +00000-0 +46935-4 0 00003
2 58069 43.0040 171.2193 0001615 272.1833 87.8834 15.27577698 09
| Epoch (UTC): | 25 May 2026 11:16:09 |
| Eccentricity: | 0.0001615 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.2193° |
| argument of perigee: | 272.1833° |
| revolutions per day: | 15.27577698 |
| mean anomaly at epoch: | 87.8834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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