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 23331.66644974 .00044084 00000-0 79556-3 0 9998
2 42778 97.1324 3.5315 0004954 207.9493 152.1493 15.49609267357941
| Epoch (UTC): | 27 November 2023 15:59:41 |
| Eccentricity: | 0.0004954 |
| inclination: | 97.1324° |
| perigee height: | 414 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 3.5315° |
| argument of perigee: | 207.9493° |
| revolutions per day: | 15.49609267 |
| mean anomaly at epoch: | 152.1493° |
| orbit number at epoch: | 35794 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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