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 25544U 98067A 22018.47812211 .00006924 00000-0 13123-3 0 9993
2 25544 51.6458 357.9712 0006626 34.7503 108.9827 15.49539245321960
| Epoch (UTC): | 18 January 2022 11:28:29 |
| Eccentricity: | 0.0006626 |
| inclination: | 51.6458° |
| perigee height: | 413 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 357.9712° |
| argument of perigee: | 34.7503° |
| revolutions per day: | 15.49539245 |
| mean anomaly at epoch: | 108.9827° |
| orbit number at epoch: | 32196 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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