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 00016U 58002A 22219.52592729 -.00000021 00000-0 -49194-4 0 9995
2 00016 34.2795 59.2230 2027095 291.2785 48.3842 10.48822721540844
| Epoch (UTC): | 07 August 2022 12:37:20 |
| Eccentricity: | 0.2027095 |
| inclination: | 34.2795° |
| perigee height: | 651 km |
| apogee height: | 4225 km |
| right ascension of ascending node: | 59.2230° |
| argument of perigee: | 291.2785° |
| revolutions per day: | 10.48822721 |
| mean anomaly at epoch: | 48.3842° |
| orbit number at epoch: | 54084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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