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 12889U 81100C 22227.36046867 .00000341 00000-0 18803-3 0 9994
2 12889 99.9115 340.6602 1315570 215.3936 173.8327 12.18235956810514
| Epoch (UTC): | 15 August 2022 08:39:04 |
| Eccentricity: | 0.1315570 |
| inclination: | 99.9115° |
| perigee height: | 550 km |
| apogee height: | 2650 km |
| right ascension of ascending node: | 340.6602° |
| argument of perigee: | 215.3936° |
| revolutions per day: | 12.18235956 |
| mean anomaly at epoch: | 173.8327° |
| orbit number at epoch: | 81051 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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