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 42833U 17042J 22222.84553444 .00000818 00000-0 85108-4 0 9994
2 42833 97.4177 74.7217 0013488 175.6320 184.5021 14.92272916276259
| Epoch (UTC): | 10 August 2022 20:17:34 |
| Eccentricity: | 0.0013488 |
| inclination: | 97.4177° |
| perigee height: | 581 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 74.7217° |
| argument of perigee: | 175.6320° |
| revolutions per day: | 14.92272916 |
| mean anomaly at epoch: | 184.5021° |
| orbit number at epoch: | 27625 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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