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 23150.13242531 -.00000215 00000-0 -88596-4 0 9995
2 23704 70.9849 169.0323 0008171 28.6802 331.4767 14.13531153422873
| Epoch (UTC): | 30 May 2023 03:10:41 |
| Eccentricity: | 0.0008171 |
| inclination: | 70.9849° |
| perigee height: | 841 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 169.0323° |
| argument of perigee: | 28.6802° |
| revolutions per day: | 14.13531153 |
| mean anomaly at epoch: | 331.4767° |
| orbit number at epoch: | 42287 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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