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 58085U 26145.31304354 +.00000000 +00000-0 +75292-4 0 00009
2 58085 43.0050 8.6276 0001426 268.9848 91.0840 15.27588452 06
| Epoch (UTC): | 25 May 2026 07:30:46 |
| Eccentricity: | 0.0001426 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.6276° |
| argument of perigee: | 268.9848° |
| revolutions per day: | 15.27588452 |
| mean anomaly at epoch: | 91.0840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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