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 22179.13516069 .00000780 00000-0 11025-3 0 9997
2 33498 98.1683 71.3182 0009748 211.3975 148.6656 14.80016754723433
| Epoch (UTC): | 28 June 2022 03:14:37 |
| Eccentricity: | 0.0009748 |
| inclination: | 98.1683° |
| perigee height: | 622 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 71.3182° |
| argument of perigee: | 211.3975° |
| revolutions per day: | 14.80016754 |
| mean anomaly at epoch: | 148.6656° |
| orbit number at epoch: | 72343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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