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 39770U 14029E 23090.34537377 .00030638 00000-0 25457-2 0 9990
2 39770 97.9569 215.5876 0010160 212.8187 147.2395 14.98631927480489
| Epoch (UTC): | 31 March 2023 08:17:20 |
| Eccentricity: | 0.0010160 |
| inclination: | 97.9569° |
| perigee height: | 564 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 215.5876° |
| argument of perigee: | 212.8187° |
| revolutions per day: | 14.98631927 |
| mean anomaly at epoch: | 147.2395° |
| orbit number at epoch: | 48048 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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