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 00005U 58002B 22022.55771106 .00000105 00000-0 15609-3 0 9990
2 00005 34.2401 228.9165 1843365 100.8944 280.3452 10.84849428268693
| Epoch (UTC): | 22 January 2022 13:23:06 |
| Eccentricity: | 0.1843365 |
| inclination: | 34.2401° |
| perigee height: | 652 km |
| apogee height: | 3830 km |
| right ascension of ascending node: | 228.9165° |
| argument of perigee: | 100.8944° |
| revolutions per day: | 10.84849428 |
| mean anomaly at epoch: | 280.3452° |
| orbit number at epoch: | 26869 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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