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 23342.89827983 .00029848 00000-0 52048-3 0 9996
2 42778 97.1330 14.6481 0006221 167.2028 192.9384 15.50655116359686
| Epoch (UTC): | 08 December 2023 21:33:31 |
| Eccentricity: | 0.0006221 |
| inclination: | 97.1330° |
| perigee height: | 410 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 14.6481° |
| argument of perigee: | 167.2028° |
| revolutions per day: | 15.50655116 |
| mean anomaly at epoch: | 192.9384° |
| orbit number at epoch: | 35968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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