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 05175U 71035B 22225.46510752 .00000090 00000-0 38045-4 0 9990
2 05175 74.0505 343.3771 0028919 85.1025 275.3429 14.38148326685370
| Epoch (UTC): | 13 August 2022 11:09:45 |
| Eccentricity: | 0.0028919 |
| inclination: | 74.0505° |
| perigee height: | 744 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 343.3771° |
| argument of perigee: | 85.1025° |
| revolutions per day: | 14.38148326 |
| mean anomaly at epoch: | 275.3429° |
| orbit number at epoch: | 68537 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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