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 12465U 81046B 22230.88378380 .00003490 00000-0 17599-3 0 9991
2 12465 81.2434 12.1214 0033865 122.5899 237.8608 15.16358663240277
| Epoch (UTC): | 18 August 2022 21:12:38 |
| Eccentricity: | 0.0033865 |
| inclination: | 81.2434° |
| perigee height: | 493 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 12.1214° |
| argument of perigee: | 122.5899° |
| revolutions per day: | 15.16358663 |
| mean anomaly at epoch: | 237.8608° |
| orbit number at epoch: | 24027 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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