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 40032U 14033Y 23033.35085350 .00004420 00000-0 44862-3 0 9997
2 40032 97.9567 332.4439 0011880 26.4329 333.7492 14.91330679467861
| Epoch (UTC): | 02 February 2023 08:25:13 |
| Eccentricity: | 0.0011880 |
| inclination: | 97.9567° |
| perigee height: | 585 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 332.4439° |
| argument of perigee: | 26.4329° |
| revolutions per day: | 14.91330679 |
| mean anomaly at epoch: | 333.7492° |
| orbit number at epoch: | 46786 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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