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 22147.81329592 .00000101 00000-0 19907-4 0 9990
2 00058 28.3274 95.8352 0165046 182.1421 177.8423 13.46335156 34279
| Epoch (UTC): | 27 May 2022 19:31:08 |
| Eccentricity: | 0.0165046 |
| inclination: | 28.3274° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 95.8352° |
| argument of perigee: | 182.1421° |
| revolutions per day: | 13.46335156 |
| mean anomaly at epoch: | 177.8423° |
| orbit number at epoch: | 3427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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