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 22136.21116304 .00018770 00000-0 83033-3 0 9992
2 37855 101.7059 238.2708 0156354 159.0899 201.6806 15.11420242576832
| Epoch (UTC): | 16 May 2022 05:04:04 |
| Eccentricity: | 0.0156354 |
| inclination: | 101.7059° |
| perigee height: | 424 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 238.2708° |
| argument of perigee: | 159.0899° |
| revolutions per day: | 15.11420242 |
| mean anomaly at epoch: | 201.6806° |
| orbit number at epoch: | 57683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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