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 42766U 17036B 23342.54894476 .00047516 00000-0 71384-3 0 9992
2 42766 97.1335 11.2761 0006420 164.2797 195.8658 15.54718673359546
| Epoch (UTC): | 08 December 2023 13:10:28 |
| Eccentricity: | 0.0006420 |
| inclination: | 97.1335° |
| perigee height: | 398 km |
| apogee height: | 407 km |
| right ascension of ascending node: | 11.2761° |
| argument of perigee: | 164.2797° |
| revolutions per day: | 15.54718673 |
| mean anomaly at epoch: | 195.8658° |
| orbit number at epoch: | 35954 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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