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 12646U 81075B 23147.84471288 .00000072 00000-0 29679-4 0 9995
2 12646 81.2250 293.9320 0066430 270.7531 196.7669 14.16027623158999
| Epoch (UTC): | 27 May 2023 20:16:23 |
| Eccentricity: | 0.0066430 |
| inclination: | 81.2250° |
| perigee height: | 791 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 293.9320° |
| argument of perigee: | 270.7531° |
| revolutions per day: | 14.16027623 |
| mean anomaly at epoch: | 196.7669° |
| orbit number at epoch: | 15899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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