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 23331.60525023 .00003387 00000-0 61963-3 0 9998
2 28895 98.1754 102.7173 0014974 277.4276 82.5226 14.66460272964753
| Epoch (UTC): | 27 November 2023 14:31:33 |
| Eccentricity: | 0.0014974 |
| inclination: | 98.1754° |
| perigee height: | 662 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 102.7173° |
| argument of perigee: | 277.4276° |
| revolutions per day: | 14.66460272 |
| mean anomaly at epoch: | 82.5226° |
| orbit number at epoch: | 96475 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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