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 58355U 26145.41284124 +.00000000 +00000-0 -12179-4 0 00008
2 58355 43.0068 277.1095 0002167 263.4466 96.6139 15.27575519 08
| Epoch (UTC): | 25 May 2026 09:54:29 |
| Eccentricity: | 0.0002167 |
| inclination: | 43.0068° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 277.1095° |
| argument of perigee: | 263.4466° |
| revolutions per day: | 15.27575519 |
| mean anomaly at epoch: | 96.6139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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