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 33498U 09002G 22178.52669087 .00000870 00000-0 12215-3 0 9990
2 33498 98.1684 70.6994 0009713 213.5219 146.5378 14.80016032722924
| Epoch (UTC): | 27 June 2022 12:38:26 |
| Eccentricity: | 0.0009713 |
| inclination: | 98.1684° |
| perigee height: | 622 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 70.6994° |
| argument of perigee: | 213.5219° |
| revolutions per day: | 14.80016032 |
| mean anomaly at epoch: | 146.5378° |
| orbit number at epoch: | 72292 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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