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 22176.78403739 .00000508 00000-0 81469-4 0 9993
2 33499 98.2172 58.9679 0007741 292.9398 67.0993 14.76028469721904
| Epoch (UTC): | 25 June 2022 18:49:00 |
| Eccentricity: | 0.0007741 |
| inclination: | 98.2172° |
| perigee height: | 636 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 58.9679° |
| argument of perigee: | 292.9398° |
| revolutions per day: | 14.76028469 |
| mean anomaly at epoch: | 67.0993° |
| orbit number at epoch: | 72190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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