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 58089U 26145.62634185 +.00000000 +00000-0 +11703-4 0 00002
2 58089 43.0048 3.2704 0001048 268.6908 91.3824 15.27579390 04
| Epoch (UTC): | 25 May 2026 15:01:55 |
| Eccentricity: | 0.0001048 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.2704° |
| argument of perigee: | 268.6908° |
| revolutions per day: | 15.27579390 |
| mean anomaly at epoch: | 91.3824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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