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 28892U 05043C 25189.38298906 .00001061 00000-0 18257-3 0 9995
2 28892 98.2616 334.5737 0013431 214.7272 145.3058 14.70656588 51206
| Epoch (UTC): | 08 July 2025 09:11:30 |
| Eccentricity: | 0.0013431 |
| inclination: | 98.2616° |
| perigee height: | 649 km |
| apogee height: | 668 km |
| right ascension of ascending node: | 334.5737° |
| argument of perigee: | 214.7272° |
| revolutions per day: | 14.70656588 |
| mean anomaly at epoch: | 145.3058° |
| orbit number at epoch: | 5120 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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