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 00058U 26083.66252773 +.00000000 +00000-0 +57608-4 0 00003
2 00058 28.3270 208.6242 0164846 227.9215 130.7202 13.46426855 07
| Epoch (UTC): | 24 March 2026 15:54:02 |
| Eccentricity: | 0.0164846 |
| inclination: | 28.3270° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 208.6242° |
| argument of perigee: | 227.9215° |
| revolutions per day: | 13.46426855 |
| mean anomaly at epoch: | 130.7202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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