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 58807U 26145.53979461 +.00000000 +00000-0 +43984-4 0 00005
2 58807 43.0005 90.8523 0000731 260.3135 99.7634 15.27570456 00
| Epoch (UTC): | 25 May 2026 12:57:18 |
| Eccentricity: | 0.0000731 |
| inclination: | 43.0005° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 90.8523° |
| argument of perigee: | 260.3135° |
| revolutions per day: | 15.27570456 |
| mean anomaly at epoch: | 99.7634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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