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 40927U 15051C 21090.23184234 .13278223 23525-5 52265-3 0 9996
2 40927 97.0132 151.3964 0010452 252.6213 145.1028 16.42992726311945
| Epoch (UTC): | 31 March 2021 05:33:51 |
| Eccentricity: | 0.0010452 |
| inclination: | 97.0132° |
| perigee height: | 151 km |
| apogee height: | 164 km |
| right ascension of ascending node: | 151.3964° |
| argument of perigee: | 252.6213° |
| revolutions per day: | 16.42992726 |
| mean anomaly at epoch: | 145.1028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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