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 22221.33700122 .00000608 00000-0 12385-3 0 9997
2 28895 98.1130 351.9211 0015990 339.2634 20.7918 14.64417785895154
| Epoch (UTC): | 09 August 2022 08:05:16 |
| Eccentricity: | 0.0015990 |
| inclination: | 98.1130° |
| perigee height: | 667 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 351.9211° |
| argument of perigee: | 339.2634° |
| revolutions per day: | 14.64417785 |
| mean anomaly at epoch: | 20.7918° |
| orbit number at epoch: | 89515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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