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 58855U 26145.43964316 +.00000000 +00000-0 -30541-4 0 00006
2 58855 43.0002 175.2119 0001181 269.7017 90.3699 15.27572971 03
| Epoch (UTC): | 25 May 2026 10:33:05 |
| Eccentricity: | 0.0001181 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.2119° |
| argument of perigee: | 269.7017° |
| revolutions per day: | 15.27572971 |
| mean anomaly at epoch: | 90.3699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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