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 23157.55670644 .00001209 00000-0 17884-3 0 9997
2 33499 98.1744 49.7377 0007332 260.8336 99.2044 14.77049915772497
| Epoch (UTC): | 06 June 2023 13:21:39 |
| Eccentricity: | 0.0007332 |
| inclination: | 98.1744° |
| perigee height: | 633 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 49.7377° |
| argument of perigee: | 260.8336° |
| revolutions per day: | 14.77049915 |
| mean anomaly at epoch: | 99.2044° |
| orbit number at epoch: | 77249 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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