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 58066U 26145.49300437 +.00000000 +00000-0 +24461-3 0 00006
2 58066 42.9991 313.5069 0001377 266.4424 93.6270 15.27589154 08
| Epoch (UTC): | 25 May 2026 11:49:55 |
| Eccentricity: | 0.0001377 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.5069° |
| argument of perigee: | 266.4424° |
| revolutions per day: | 15.27589154 |
| mean anomaly at epoch: | 93.6270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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