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 22182.81734691 .00000287 00000-0 49430-4 0 9994
2 33499 98.2162 65.1005 0007618 270.2506 89.7830 14.76033838722367
| Epoch (UTC): | 01 July 2022 19:36:58 |
| Eccentricity: | 0.0007618 |
| inclination: | 98.2162° |
| perigee height: | 636 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 65.1005° |
| argument of perigee: | 270.2506° |
| revolutions per day: | 14.76033838 |
| mean anomaly at epoch: | 89.7830° |
| orbit number at epoch: | 72236 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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