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 33683U 99025DFU 23082.38564980 .00013973 00000-0 34948-2 0 9999
2 33683 98.2450 292.7593 0066053 336.2587 23.5564 14.50257116784493
| Epoch (UTC): | 23 March 2023 09:15:20 |
| Eccentricity: | 0.0066053 |
| inclination: | 98.2450° |
| perigee height: | 678 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 292.7593° |
| argument of perigee: | 336.2587° |
| revolutions per day: | 14.50257116 |
| mean anomaly at epoch: | 23.5564° |
| orbit number at epoch: | 78449 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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