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 42777U 17036N 23175.15373253 .15930252 24069-5 31628-3 0 9997
2 42777 97.1065 222.4278 0014006 253.4659 106.5106 16.46095853334667
| Epoch (UTC): | 24 June 2023 03:41:22 |
| Eccentricity: | 0.0014006 |
| inclination: | 97.1065° |
| perigee height: | 140 km |
| apogee height: | 159 km |
| right ascension of ascending node: | 222.4278° |
| argument of perigee: | 253.4659° |
| revolutions per day: | 16.46095853 |
| mean anomaly at epoch: | 106.5106° |
| orbit number at epoch: | 33466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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