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 23086.82235883 .00002838 00000-0 53419-3 0 9998
2 28895 98.1388 219.5856 0015549 331.9829 28.0535 14.65297882928897
| Epoch (UTC): | 27 March 2023 19:44:11 |
| Eccentricity: | 0.0015549 |
| inclination: | 98.1388° |
| perigee height: | 665 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 219.5856° |
| argument of perigee: | 331.9829° |
| revolutions per day: | 14.65297882 |
| mean anomaly at epoch: | 28.0535° |
| orbit number at epoch: | 92889 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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