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 33312U 08040A 22176.91265690 .00001319 00000-0 12024-3 0 9996
2 33312 97.5949 235.7711 0013454 72.2399 288.0290 14.96729866748165
| Epoch (UTC): | 25 June 2022 21:54:13 |
| Eccentricity: | 0.0013454 |
| inclination: | 97.5949° |
| perigee height: | 567 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 235.7711° |
| argument of perigee: | 72.2399° |
| revolutions per day: | 14.96729866 |
| mean anomaly at epoch: | 288.0290° |
| orbit number at epoch: | 74816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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