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 39161U 13021C 23080.11512288 .00003244 00000-0 50188-3 0 9996
2 39161 97.8800 154.8821 0008162 251.4741 108.5566 14.73891652530201
| Epoch (UTC): | 21 March 2023 02:45:46 |
| Eccentricity: | 0.0008162 |
| inclination: | 97.8800° |
| perigee height: | 643 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 154.8821° |
| argument of perigee: | 251.4741° |
| revolutions per day: | 14.73891652 |
| mean anomaly at epoch: | 108.5566° |
| orbit number at epoch: | 53020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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