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 23153.32091685 -.00000104 00000-0 -28576-4 0 9997
2 19650 70.9979 119.0575 0012219 114.5128 245.7270 14.15890259783727
| Epoch (UTC): | 02 June 2023 07:42:07 |
| Eccentricity: | 0.0012219 |
| inclination: | 70.9979° |
| perigee height: | 830 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 119.0575° |
| argument of perigee: | 114.5128° |
| revolutions per day: | 14.15890259 |
| mean anomaly at epoch: | 245.7270° |
| orbit number at epoch: | 78372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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