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 22176.39431932 .00000010 00000-0 35792-4 0 9995
2 00016 34.2582 183.7882 2026099 109.3766 273.6000 10.48823545536316
| Epoch (UTC): | 25 June 2022 09:27:49 |
| Eccentricity: | 0.2026099 |
| inclination: | 34.2582° |
| perigee height: | 651 km |
| apogee height: | 4224 km |
| right ascension of ascending node: | 183.7882° |
| argument of perigee: | 109.3766° |
| revolutions per day: | 10.48823545 |
| mean anomaly at epoch: | 273.6000° |
| orbit number at epoch: | 53631 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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