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 42017U 17008BX 23092.13008322 .00120144 00000-0 16104-2 0 9991
2 42017 97.2225 161.3564 0003117 252.2150 107.8766 15.57557374341550
| Epoch (UTC): | 02 April 2023 03:07:19 |
| Eccentricity: | 0.0003117 |
| inclination: | 97.2225° |
| perigee height: | 392 km |
| apogee height: | 397 km |
| right ascension of ascending node: | 161.3564° |
| argument of perigee: | 252.2150° |
| revolutions per day: | 15.57557374 |
| mean anomaly at epoch: | 107.8766° |
| orbit number at epoch: | 34155 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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