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 31766U 99025CFR 23031.76965662 .00000269 00000-0 19123-3 0 9990
2 31766 98.8190 48.8212 0074744 341.6331 18.2141 14.04359299494002
| Epoch (UTC): | 31 January 2023 18:28:18 |
| Eccentricity: | 0.0074744 |
| inclination: | 98.8190° |
| perigee height: | 824 km |
| apogee height: | 933 km |
| right ascension of ascending node: | 48.8212° |
| argument of perigee: | 341.6331° |
| revolutions per day: | 14.04359299 |
| mean anomaly at epoch: | 18.2141° |
| orbit number at epoch: | 49400 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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