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 37855U 11061F 22179.55166866 .00005063 00000-0 22501-3 0 9998
2 37855 101.7109 304.4990 0152584 29.1218 331.8401 15.12578726582915
| Epoch (UTC): | 28 June 2022 13:14:24 |
| Eccentricity: | 0.0152584 |
| inclination: | 101.7109° |
| perigee height: | 423 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 304.4990° |
| argument of perigee: | 29.1218° |
| revolutions per day: | 15.12578726 |
| mean anomaly at epoch: | 331.8401° |
| orbit number at epoch: | 58291 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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