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 00058U 60013A 22146.55283396 .00000098 00000-0 17047-4 0 9999
2 00058 28.3270 102.2298 0165043 171.7056 188.6266 13.46335093 34109
| Epoch (UTC): | 26 May 2022 13:16:04 |
| Eccentricity: | 0.0165043 |
| inclination: | 28.3270° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 102.2298° |
| argument of perigee: | 171.7056° |
| revolutions per day: | 13.46335093 |
| mean anomaly at epoch: | 188.6266° |
| orbit number at epoch: | 3410 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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