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 58875U 26145.43449895 +.00000000 +00000-0 +19208-4 0 00004
2 58875 43.0008 175.1550 0001258 273.9491 86.1217 15.27577339 09
| Epoch (UTC): | 25 May 2026 10:25:40 |
| Eccentricity: | 0.0001258 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.1550° |
| argument of perigee: | 273.9491° |
| revolutions per day: | 15.27577339 |
| mean anomaly at epoch: | 86.1217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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