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 12849U 81094B 22144.21802584 .00001265 00000-0 11820-3 0 9998
2 12849 82.4947 222.8487 0897034 246.2691 104.1920 13.51332798985173
| Epoch (UTC): | 24 May 2022 05:13:57 |
| Eccentricity: | 0.0897034 |
| inclination: | 82.4947° |
| perigee height: | 399 km |
| apogee height: | 1735 km |
| right ascension of ascending node: | 222.8487° |
| argument of perigee: | 246.2691° |
| revolutions per day: | 13.51332798 |
| mean anomaly at epoch: | 104.1920° |
| orbit number at epoch: | 98517 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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