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 14781U 84021B 22342.36644251 .00001164 00000-0 14570-3 0 9992
2 14781 97.6361 322.0788 0009789 106.3589 253.8703 14.84016291 65836
| Epoch (UTC): | 08 December 2022 08:47:40 |
| Eccentricity: | 0.0009789 |
| inclination: | 97.6361° |
| perigee height: | 610 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 322.0788° |
| argument of perigee: | 106.3589° |
| revolutions per day: | 14.84016291 |
| mean anomaly at epoch: | 253.8703° |
| orbit number at epoch: | 6583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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