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 58096U 26145.64304110 +.00000000 +00000-0 +68376-4 0 00002
2 58096 43.0028 3.3813 0001624 263.8894 96.1773 15.27579688 09
| Epoch (UTC): | 25 May 2026 15:25:58 |
| Eccentricity: | 0.0001624 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.3813° |
| argument of perigee: | 263.8894° |
| revolutions per day: | 15.27579688 |
| mean anomaly at epoch: | 96.1773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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