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 29499U 06044A 18171.96649306 -.00000009 +00000-0 +15665-4 0 9995
2 29499 098.6264 229.3640 0001445 136.3470 205.8982 14.21524487605344
| Epoch (UTC): | 20 June 2018 23:11:45 |
| Eccentricity: | 0.0001445 |
| inclination: | 98.6264° |
| perigee height: | 819 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 229.3640° |
| argument of perigee: | 136.3470° |
| revolutions per day: | 14.21524487 |
| mean anomaly at epoch: | 205.8982° |
| orbit number at epoch: | 60534 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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