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 23159.40275960 -.00000309 00000-0 -13878-3 0 9990
2 23704 70.9839 149.5979 0008669 13.7632 346.3724 14.13527322423984
| Epoch (UTC): | 08 June 2023 09:39:58 |
| Eccentricity: | 0.0008669 |
| inclination: | 70.9839° |
| perigee height: | 841 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 149.5979° |
| argument of perigee: | 13.7632° |
| revolutions per day: | 14.13527322 |
| mean anomaly at epoch: | 346.3724° |
| orbit number at epoch: | 42398 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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