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 58007U 26145.41404645 +.00000000 +00000-0 +36700-4 0 00009
2 58007 43.0023 125.0797 0001229 260.2935 99.7778 15.27579663 04
| Epoch (UTC): | 25 May 2026 09:56:13 |
| Eccentricity: | 0.0001229 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 125.0797° |
| argument of perigee: | 260.2935° |
| revolutions per day: | 15.27579663 |
| mean anomaly at epoch: | 99.7778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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