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 data is extracted from the following two-line orbital elements,
1 23705U 95058B 22146.49769041 -.00000045 00000-0 11386-5 0 9993
2 23705 71.0211 203.3541 0010524 63.1918 297.0280 14.15171567372142
| Epoch (UTC): | 26 May 2022 11:56:40 |
| Eccentricity: | 0.0010524 |
| inclination: | 71.0211° |
| perigee height: | 834 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 203.3541° |
| argument of perigee: | 63.1918° |
| revolutions per day: | 14.15171567 |
| mean anomaly at epoch: | 297.0280° |
| orbit number at epoch: | 37214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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