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 19650U 88102B 23151.20147474 -.00000168 00000-0 -61120-4 0 9992
2 19650 70.9978 123.5151 0012208 118.3079 241.9277 14.15890603783707
| Epoch (UTC): | 31 May 2023 04:50:07 |
| Eccentricity: | 0.0012208 |
| inclination: | 70.9978° |
| perigee height: | 830 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 123.5151° |
| argument of perigee: | 118.3079° |
| revolutions per day: | 14.15890603 |
| mean anomaly at epoch: | 241.9277° |
| orbit number at epoch: | 78370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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