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 22143.71165586 .00001952 00000-0 24453-3 0 9998
2 00107 28.7848 156.3890 0542507 73.3533 292.5870 14.10057301 65800
| Epoch (UTC): | 23 May 2022 17:04:47 |
| Eccentricity: | 0.0542507 |
| inclination: | 28.7848° |
| perigee height: | 466 km |
| apogee height: | 1252 km |
| right ascension of ascending node: | 156.3890° |
| argument of perigee: | 73.3533° |
| revolutions per day: | 14.10057301 |
| mean anomaly at epoch: | 292.5870° |
| orbit number at epoch: | 6580 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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