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 58820U 26145.59616476 +.00000000 +00000-0 +50617-3 0 00000
2 58820 97.4476 240.0054 0007904 132.9283 227.2634 15.53385941 05
| Epoch (UTC): | 25 May 2026 14:18:28 |
| Eccentricity: | 0.0007904 |
| inclination: | 97.4476° |
| perigee height: | 401 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 240.0054° |
| argument of perigee: | 132.9283° |
| revolutions per day: | 15.53385941 |
| mean anomaly at epoch: | 227.2634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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