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 44829U 19084F 20301.42013769 +.04858171 +22528-5 +11601-2 0 9996
2 44829 096.9280 173.1516 0002970 147.7503 212.3975 16.29630918051372
| Epoch (UTC): | 27 October 2020 10:04:59 |
| Eccentricity: | 0.0002970 |
| inclination: | 96.9280° |
| perigee height: | 191 km |
| apogee height: | 195 km |
| right ascension of ascending node: | 173.1516° |
| argument of perigee: | 147.7503° |
| revolutions per day: | 16.29630918 |
| mean anomaly at epoch: | 212.3975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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