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 46320U 20061BA 22183.92000662 .00002162 00000-0 12667-3 0 9991
2 46320 97.4471 254.0675 0004624 99.7139 15.0523 15.12837889100865
| Epoch (UTC): | 02 July 2022 22:04:48 |
| Eccentricity: | 0.0004624 |
| inclination: | 97.4471° |
| perigee height: | 524 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 254.0675° |
| argument of perigee: | 99.7139° |
| revolutions per day: | 15.12837889 |
| mean anomaly at epoch: | 15.0523° |
| orbit number at epoch: | 10086 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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