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 28706U 90017C 22332.44278847 .00000754 00000-0 65023-3 0 9991
2 28706 83.0881 342.2355 0084700 124.0607 236.8632 13.83586848878485
| Epoch (UTC): | 28 November 2022 10:37:36 |
| Eccentricity: | 0.0084700 |
| inclination: | 83.0881° |
| perigee height: | 889 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 342.2355° |
| argument of perigee: | 124.0607° |
| revolutions per day: | 13.83586848 |
| mean anomaly at epoch: | 236.8632° |
| orbit number at epoch: | 87848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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