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 23150.07110602 -.00000196 00000-0 -75230-4 0 9997
2 19650 70.9977 125.8926 0012224 120.3617 239.8716 14.15890813783549
| Epoch (UTC): | 30 May 2023 01:42:23 |
| Eccentricity: | 0.0012224 |
| inclination: | 70.9977° |
| perigee height: | 830 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 125.8926° |
| argument of perigee: | 120.3617° |
| revolutions per day: | 14.15890813 |
| mean anomaly at epoch: | 239.8716° |
| orbit number at epoch: | 78354 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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