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 29228U 06021A 18294.43495800 .00000090 00000-0 14204-4 0 9993
2 29228 69.9345 288.0135 0007526 293.1866 66.8502 15.02368137681876
| Epoch (UTC): | 21 October 2018 10:26:20 |
| Eccentricity: | 0.0007526 |
| inclination: | 69.9345° |
| perigee height: | 554 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 288.0135° |
| argument of perigee: | 293.1866° |
| revolutions per day: | 15.02368137 |
| mean anomaly at epoch: | 66.8502° |
| orbit number at epoch: | 68187 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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