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 31598U 07023A 23028.14454709 -.00000904 00000-0 -10709-3 0 9992
2 31598 97.8881 213.6189 0001415 84.6917 275.4646 14.82141120846247
| Epoch (UTC): | 28 January 2023 03:28:08 |
| Eccentricity: | 0.0001415 |
| inclination: | 97.8881° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 213.6189° |
| argument of perigee: | 84.6917° |
| revolutions per day: | 14.82141120 |
| mean anomaly at epoch: | 275.4646° |
| orbit number at epoch: | 84624 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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