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 23704U 95058A 23150.48625449 -.00000214 00000-0 -88430-4 0 9992
2 23704 70.9849 168.2905 0008188 28.0159 332.1402 14.13531018422725
| Epoch (UTC): | 30 May 2023 11:40:12 |
| Eccentricity: | 0.0008188 |
| inclination: | 70.9849° |
| perigee height: | 841 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 168.2905° |
| argument of perigee: | 28.0159° |
| revolutions per day: | 14.13531018 |
| mean anomaly at epoch: | 332.1402° |
| orbit number at epoch: | 42272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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