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 23223U 94054A 22262.94243646 0.00000000 00000-0 00000-0 0 09
2 23223 12.5259 19.9087 0034490 106.6325 253.7643 1.00270000 05
| Epoch (UTC): | 19 September 2022 22:37:06 |
| Eccentricity: | 0.0034490 |
| inclination: | 12.5259° |
| perigee height: | 35641 km |
| apogee height: | 35932 km |
| right ascension of ascending node: | 19.9087° |
| argument of perigee: | 106.6325° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 253.7643° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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