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 24278U 96046B 22135.89846160 -.00000040 00000-0 -47318-5 0 9997
2 24278 98.5190 164.0580 0350444 7.9643 352.6865 13.53114624271207
| Epoch (UTC): | 15 May 2022 21:33:47 |
| Eccentricity: | 0.0350444 |
| inclination: | 98.5190° |
| perigee height: | 800 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 164.0580° |
| argument of perigee: | 7.9643° |
| revolutions per day: | 13.53114624 |
| mean anomaly at epoch: | 352.6865° |
| orbit number at epoch: | 27120 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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