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 23152.46769825 -.00000233 00000-0 -98139-4 0 9997
2 23704 70.9847 164.1368 0008293 24.6595 335.4922 14.13530321423005
| Epoch (UTC): | 01 June 2023 11:13:29 |
| Eccentricity: | 0.0008293 |
| inclination: | 70.9847° |
| perigee height: | 841 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 164.1368° |
| argument of perigee: | 24.6595° |
| revolutions per day: | 14.13530321 |
| mean anomaly at epoch: | 335.4922° |
| orbit number at epoch: | 42300 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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