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 23152.89702831 -.00000116 00000-0 -34418-4 0 9995
2 19650 70.9979 119.9490 0012218 115.2989 244.9401 14.15890366783663
| Epoch (UTC): | 01 June 2023 21:31:43 |
| Eccentricity: | 0.0012218 |
| inclination: | 70.9979° |
| perigee height: | 830 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 119.9490° |
| argument of perigee: | 115.2989° |
| revolutions per day: | 14.15890366 |
| mean anomaly at epoch: | 244.9401° |
| orbit number at epoch: | 78366 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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