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 58870U 26145.36525898 +.00000000 +00000-0 +47409-4 0 00003
2 58870 43.0007 175.4963 0001227 270.7719 89.2992 15.27579802 09
| Epoch (UTC): | 25 May 2026 08:45:58 |
| Eccentricity: | 0.0001227 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.4963° |
| argument of perigee: | 270.7719° |
| revolutions per day: | 15.27579802 |
| mean anomaly at epoch: | 89.2992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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