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 42778U 17036P 23333.60356893 .00051364 00000-0 91901-3 0 9991
2 42778 97.1319 5.4473 0005212 200.8042 159.2998 15.49818938358240
| Epoch (UTC): | 29 November 2023 14:29:08 |
| Eccentricity: | 0.0005212 |
| inclination: | 97.1319° |
| perigee height: | 414 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 5.4473° |
| argument of perigee: | 200.8042° |
| revolutions per day: | 15.49818938 |
| mean anomaly at epoch: | 159.2998° |
| orbit number at epoch: | 35824 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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