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 31464U 99025BVC 22222.35210826 .00000287 00000-0 18436-3 0 9992
2 31464 98.9589 266.8171 0046446 92.1283 328.1820 14.10422049774658
| Epoch (UTC): | 10 August 2022 08:27:02 |
| Eccentricity: | 0.0046446 |
| inclination: | 98.9589° |
| perigee height: | 824 km |
| apogee height: | 891 km |
| right ascension of ascending node: | 266.8171° |
| argument of perigee: | 92.1283° |
| revolutions per day: | 14.10422049 |
| mean anomaly at epoch: | 328.1820° |
| orbit number at epoch: | 77465 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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