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 31794U 07029C 22222.28710439 .00000057 00000-0 94507-4 0 9997
2 31794 71.0428 160.5516 0204908 148.0299 4.4167 13.71180531756446
| Epoch (UTC): | 10 August 2022 06:53:25 |
| Eccentricity: | 0.0204908 |
| inclination: | 71.0428° |
| perigee height: | 844 km |
| apogee height: | 1146 km |
| right ascension of ascending node: | 160.5516° |
| argument of perigee: | 148.0299° |
| revolutions per day: | 13.71180531 |
| mean anomaly at epoch: | 4.4167° |
| orbit number at epoch: | 75644 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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