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 00107U 61013A 22220.94091790 .00002509 00000-0 31956-3 0 9999
2 00107 28.7871 79.4232 0541585 61.0818 304.2982 14.10219776 76719
| Epoch (UTC): | 08 August 2022 22:34:55 |
| Eccentricity: | 0.0541585 |
| inclination: | 28.7871° |
| perigee height: | 466 km |
| apogee height: | 1250 km |
| right ascension of ascending node: | 79.4232° |
| argument of perigee: | 61.0818° |
| revolutions per day: | 14.10219776 |
| mean anomaly at epoch: | 304.2982° |
| orbit number at epoch: | 7671 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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