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 22179.81625914 .00004638 00000-0 20674-3 0 9997
2 37855 101.7110 304.9036 0152577 28.3371 332.6039 15.12581261583427
| Epoch (UTC): | 28 June 2022 19:35:24 |
| Eccentricity: | 0.0152577 |
| inclination: | 101.7110° |
| perigee height: | 423 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 304.9036° |
| argument of perigee: | 28.3371° |
| revolutions per day: | 15.12581261 |
| mean anomaly at epoch: | 332.6039° |
| orbit number at epoch: | 58342 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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