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 22220U 92076B 24255.06497811 .00000353 00000-0 20027-3 0 9991
2 22220 70.9975 255.4988 0013980 213.9167 203.1096 14.16695438645023
| Epoch (UTC): | 11 September 2024 01:33:34 |
| Eccentricity: | 0.0013980 |
| inclination: | 70.9975° |
| perigee height: | 826 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 255.4988° |
| argument of perigee: | 213.9167° |
| revolutions per day: | 14.16695438 |
| mean anomaly at epoch: | 203.1096° |
| orbit number at epoch: | 64502 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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