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 39462U 13072A 23087.10968031 0.00000000 00000-0 00000-0 0 08
2 39462 122.9934 332.5593 0003551 135.4918 224.4468 13.41451024 06
| Epoch (UTC): | 28 March 2023 02:37:56 |
| Eccentricity: | 0.0003551 |
| inclination: | 122.9934° |
| perigee height: | 1101 km |
| apogee height: | 1106 km |
| right ascension of ascending node: | 332.5593° |
| argument of perigee: | 135.4918° |
| revolutions per day: | 13.41451024 |
| mean anomaly at epoch: | 224.4468° |
| 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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