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 is defined by the following mean orbital elements,
1 39403U 13064Z 21237.42839327 .03236251 72087-5 59674-3 0 9991
2 39403 40.4990 292.7885 0004167 65.7366 294.3916 16.31224824436852
| Epoch (UTC): | 25 August 2021 10:16:53 |
| Eccentricity: | 0.0004167 |
| inclination: | 40.4990° |
| perigee height: | 186 km |
| apogee height: | 192 km |
| right ascension of ascending node: | 292.7885° |
| argument of perigee: | 65.7366° |
| revolutions per day: | 16.31224824 |
| mean anomaly at epoch: | 294.3916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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