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 22024.86129019 .00000092 00000-0 11166-3 0 9997
2 00016 34.2647 261.4245 2026740 190.3136 164.8855 10.48801080520401
| Epoch (UTC): | 24 January 2022 20:40:15 |
| Eccentricity: | 0.2026740 |
| inclination: | 34.2647° |
| perigee height: | 651 km |
| apogee height: | 4224 km |
| right ascension of ascending node: | 261.4245° |
| argument of perigee: | 190.3136° |
| revolutions per day: | 10.48801080 |
| mean anomaly at epoch: | 164.8855° |
| orbit number at epoch: | 52040 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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