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 71000C 21999A 21047.21097720 .00000770 00000-0 12948-5 0 06
2 71000 53.0560 103.0494 0024061 218.0896 57.6311 16.01463293 16
| Epoch (UTC): | 16 February 2021 05:03:48 |
| Eccentricity: | 0.0024061 |
| inclination: | 53.0560° |
| perigee height: | 254 km |
| apogee height: | 286 km |
| right ascension of ascending node: | 103.0494° |
| argument of perigee: | 218.0896° |
| revolutions per day: | 16.01463293 |
| mean anomaly at epoch: | 57.6311° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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