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 23083.33973321 .00009542 00000-0 17729-2 0 9999
2 28895 98.1386 216.1375 0015796 343.3841 16.6842 14.65295546928382
| Epoch (UTC): | 24 March 2023 08:09:12 |
| Eccentricity: | 0.0015796 |
| inclination: | 98.1386° |
| perigee height: | 665 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 216.1375° |
| argument of perigee: | 343.3841° |
| revolutions per day: | 14.65295546 |
| mean anomaly at epoch: | 16.6842° |
| orbit number at epoch: | 92838 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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