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 37232U 10063A 21250.10315226 0.00000000 00000-0 00000-0 0 00
2 37232 5.1064 118.9826 0034205 182.3602 177.6368 1.00270000 04
| Epoch (UTC): | 07 September 2021 02:28:32 |
| Eccentricity: | 0.0034205 |
| inclination: | 5.1064° |
| perigee height: | 35642 km |
| apogee height: | 35931 km |
| right ascension of ascending node: | 118.9826° |
| argument of perigee: | 182.3602° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 177.6368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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