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 58627U 26145.58154956 +.00000000 +00000-0 -69395-4 0 00009
2 58627 43.0018 352.6291 0001162 253.3988 106.6736 15.27596306 05
| Epoch (UTC): | 25 May 2026 13:57:25 |
| Eccentricity: | 0.0001162 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.6291° |
| argument of perigee: | 253.3988° |
| revolutions per day: | 15.27596306 |
| mean anomaly at epoch: | 106.6736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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