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 44830U 19084G 20283.37625441 +.14504533 +23319-5 +28099-3 0 9997
2 44830 096.9282 155.2233 0011473 239.9810 120.0357 16.46538413048546
| Epoch (UTC): | 09 October 2020 09:01:48 |
| Eccentricity: | 0.0011473 |
| inclination: | 96.9282° |
| perigee height: | 141 km |
| apogee height: | 156 km |
| right ascension of ascending node: | 155.2233° |
| argument of perigee: | 239.9810° |
| revolutions per day: | 16.46538413 |
| mean anomaly at epoch: | 120.0357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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