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 33495U 09002D 21332.07805678 .00000052 00000-0 16603-4 0 9994
2 33495 98.3108 193.6395 0006875 286.7167 73.3285 14.72255571689903
| Epoch (UTC): | 28 November 2021 01:52:24 |
| Eccentricity: | 0.0006875 |
| inclination: | 98.3108° |
| perigee height: | 649 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 193.6395° |
| argument of perigee: | 286.7167° |
| revolutions per day: | 14.72255571 |
| mean anomaly at epoch: | 73.3285° |
| orbit number at epoch: | 68990 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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