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 28895U 05043F 22180.88659214 .00000432 00000-0 90699-4 0 9996
2 28895 98.1084 312.0741 0018020 101.9275 258.3949 14.64364856889235
| Epoch (UTC): | 29 June 2022 21:16:41 |
| Eccentricity: | 0.0018020 |
| inclination: | 98.1084° |
| perigee height: | 666 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 312.0741° |
| argument of perigee: | 101.9275° |
| revolutions per day: | 14.64364856 |
| mean anomaly at epoch: | 258.3949° |
| orbit number at epoch: | 88923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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