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 23154.30999006 -.00000050 00000-0 -91505-6 0 9994
2 19650 70.9980 116.9772 0012225 112.7614 247.4802 14.15890246783862
| Epoch (UTC): | 03 June 2023 07:26:23 |
| Eccentricity: | 0.0012225 |
| inclination: | 70.9980° |
| perigee height: | 830 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 116.9772° |
| argument of perigee: | 112.7614° |
| revolutions per day: | 14.15890246 |
| mean anomaly at epoch: | 247.4802° |
| orbit number at epoch: | 78386 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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