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 23153.45842040 -.00000238 00000-0 -10095-3 0 9997
2 23704 70.9846 162.0598 0008347 22.9970 337.1523 14.13530007423146
| Epoch (UTC): | 02 June 2023 11:00:07 |
| Eccentricity: | 0.0008347 |
| inclination: | 70.9846° |
| perigee height: | 841 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 162.0598° |
| argument of perigee: | 22.9970° |
| revolutions per day: | 14.13530007 |
| mean anomaly at epoch: | 337.1523° |
| orbit number at epoch: | 42314 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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