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 58482U 26145.57310612 +.00000000 +00000-0 +56862-3 0 00003
2 58482 43.0010 349.4938 0001683 254.3884 105.6782 15.27590848 07
| Epoch (UTC): | 25 May 2026 13:45:16 |
| Eccentricity: | 0.0001683 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 349.4938° |
| argument of perigee: | 254.3884° |
| revolutions per day: | 15.27590848 |
| mean anomaly at epoch: | 105.6782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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