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 22178.54657925 .00000478 00000-0 77219-4 0 9991
2 33499 98.2169 60.7595 0007683 286.3447 73.6917 14.76030508721732
| Epoch (UTC): | 27 June 2022 13:07:04 |
| Eccentricity: | 0.0007683 |
| inclination: | 98.2169° |
| perigee height: | 636 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 60.7595° |
| argument of perigee: | 286.3447° |
| revolutions per day: | 14.76030508 |
| mean anomaly at epoch: | 73.6917° |
| orbit number at epoch: | 72173 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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