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 22181.59240999 .00000526 00000-0 50862-4 0 9993
2 33312 97.5949 240.3160 0013310 57.7220 302.5289 14.96739112748869
| Epoch (UTC): | 30 June 2022 14:13:04 |
| Eccentricity: | 0.0013310 |
| inclination: | 97.5949° |
| perigee height: | 568 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 240.3160° |
| argument of perigee: | 57.7220° |
| revolutions per day: | 14.96739112 |
| mean anomaly at epoch: | 302.5289° |
| orbit number at epoch: | 74886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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