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 28366U 04025A 21025.38943275 .00000023 00000-0 20696-4 0 9999
2 28366 98.2392 273.2954 0108739 61.8027 299.4091 14.36726093868865
| Epoch (UTC): | 25 January 2021 09:20:46 |
| Eccentricity: | 0.0108739 |
| inclination: | 98.2392° |
| perigee height: | 691 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 273.2954° |
| argument of perigee: | 61.8027° |
| revolutions per day: | 14.36726093 |
| mean anomaly at epoch: | 299.4091° |
| orbit number at epoch: | 86886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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