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 28894U 05043E 23266.30286064 .00001268 00000-0 25822-3 0 9990
2 28894 98.1782 29.8661 0017024 164.3906 195.7824 14.62659288954277
| Epoch (UTC): | 23 September 2023 07:16:07 |
| Eccentricity: | 0.0017024 |
| inclination: | 98.1782° |
| perigee height: | 672 km |
| apogee height: | 696 km |
| right ascension of ascending node: | 29.8661° |
| argument of perigee: | 164.3906° |
| revolutions per day: | 14.62659288 |
| mean anomaly at epoch: | 195.7824° |
| orbit number at epoch: | 95427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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