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 33499U 09002H 22179.90237945 .00000397 00000-0 65380-4 0 9994
2 33499 98.2167 62.1376 0007647 281.2105 78.8244 14.76031649721937
| Epoch (UTC): | 28 June 2022 21:39:25 |
| Eccentricity: | 0.0007647 |
| inclination: | 98.2167° |
| perigee height: | 636 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 62.1376° |
| argument of perigee: | 281.2105° |
| revolutions per day: | 14.76031649 |
| mean anomaly at epoch: | 78.8244° |
| orbit number at epoch: | 72193 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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