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 23031.23997841 -.00000194 00000-0 -74182-4 0 9994
2 19650 71.0007 15.8057 0016639 292.5598 67.3764 14.15862706766449
| Epoch (UTC): | 31 January 2023 05:45:34 |
| Eccentricity: | 0.0016639 |
| inclination: | 71.0007° |
| perigee height: | 827 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 15.8057° |
| argument of perigee: | 292.5598° |
| revolutions per day: | 14.15862706 |
| mean anomaly at epoch: | 67.3764° |
| orbit number at epoch: | 76644 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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