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 23277.60067255 .00043840 00000-0 92853-3 0 9996
2 42778 97.1421 310.2180 0008795 73.0201 287.2012 15.44936998349580
| Epoch (UTC): | 04 October 2023 14:24:58 |
| Eccentricity: | 0.0008795 |
| inclination: | 97.1421° |
| perigee height: | 425 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 310.2180° |
| argument of perigee: | 73.0201° |
| revolutions per day: | 15.44936998 |
| mean anomaly at epoch: | 287.2012° |
| orbit number at epoch: | 34958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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