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 58195U 26145.47967071 +.00000000 +00000-0 -19842-3 0 00008
2 58195 43.0086 69.3416 0001764 272.8076 87.2574 15.27606816 05
| Epoch (UTC): | 25 May 2026 11:30:43 |
| Eccentricity: | 0.0001764 |
| inclination: | 43.0086° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.3416° |
| argument of perigee: | 272.8076° |
| revolutions per day: | 15.27606816 |
| mean anomaly at epoch: | 87.2574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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