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 58360U 26145.11491014 +.00000000 +00000-0 -94843-5 0 00008
2 58360 43.0018 293.6296 0001284 267.0611 93.0094 15.27573871 06
| Epoch (UTC): | 25 May 2026 02:45:28 |
| Eccentricity: | 0.0001284 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 293.6296° |
| argument of perigee: | 267.0611° |
| revolutions per day: | 15.27573871 |
| mean anomaly at epoch: | 93.0094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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