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 28654U 05018A 22142.14304195 .00000245 00000-0 15619-3 0 9993
2 28654 98.9498 212.5987 0014959 49.7277 310.5200 14.12731576876359
| Epoch (UTC): | 22 May 2022 03:25:58 |
| Eccentricity: | 0.0014959 |
| inclination: | 98.9498° |
| perigee height: | 839 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 212.5987° |
| argument of perigee: | 49.7277° |
| revolutions per day: | 14.12731576 |
| mean anomaly at epoch: | 310.5200° |
| orbit number at epoch: | 87635 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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