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 23161.07802639 .00023031 00000-0 60574-3 0 9997
2 42778 97.1556 196.0914 0010453 123.1343 237.0908 15.38521135331632
| Epoch (UTC): | 10 June 2023 01:52:21 |
| Eccentricity: | 0.0010453 |
| inclination: | 97.1556° |
| perigee height: | 443 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 196.0914° |
| argument of perigee: | 123.1343° |
| revolutions per day: | 15.38521135 |
| mean anomaly at epoch: | 237.0908° |
| orbit number at epoch: | 33163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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