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 22181.16689849 .00000108 00000-0 82387-4 0 9995
2 28654 98.9487 251.5927 0013197 297.2889 62.6938 14.12747362881861
| Epoch (UTC): | 30 June 2022 04:00:20 |
| Eccentricity: | 0.0013197 |
| inclination: | 98.9487° |
| perigee height: | 840 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 251.5927° |
| argument of perigee: | 297.2889° |
| revolutions per day: | 14.12747362 |
| mean anomaly at epoch: | 62.6938° |
| orbit number at epoch: | 88186 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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