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 32789U 08021G 21023.56368407 .00001304 00000-0 87660-4 0 9996
2 32789 97.3944 64.4261 0010348 281.5289 78.4778 15.08415279694980
| Epoch (UTC): | 23 January 2021 13:31:42 |
| Eccentricity: | 0.0010348 |
| inclination: | 97.3944° |
| perigee height: | 534 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 64.4261° |
| argument of perigee: | 281.5289° |
| revolutions per day: | 15.08415279 |
| mean anomaly at epoch: | 78.4778° |
| orbit number at epoch: | 69498 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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