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 28538U 05004B 22141.86693391 0.00000030 00000-0 48644-4 0 06
2 28538 63.8204 80.1509 0157843 344.8105 15.1895 13.43162610 03
| Epoch (UTC): | 21 May 2022 20:48:23 |
| Eccentricity: | 0.0157843 |
| inclination: | 63.8204° |
| perigee height: | 979 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 80.1509° |
| argument of perigee: | 344.8105° |
| revolutions per day: | 13.43162610 |
| mean anomaly at epoch: | 15.1895° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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