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 31793U 07029B 22228.87027979 .00000200 00000-0 12922-3 0 9997
2 31793 70.9762 25.9376 0001918 254.7722 257.3066 14.14476579781403
| Epoch (UTC): | 16 August 2022 20:53:12 |
| Eccentricity: | 0.0001918 |
| inclination: | 70.9762° |
| perigee height: | 843 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 25.9376° |
| argument of perigee: | 254.7722° |
| revolutions per day: | 14.14476579 |
| mean anomaly at epoch: | 257.3066° |
| orbit number at epoch: | 78140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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