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 40034U 14033AA 23083.47448536 .00007600 00000-0 10666-2 0 9993
2 40034 97.6665 263.0533 0055491 329.7595 30.0417 14.76642029471286
| Epoch (UTC): | 24 March 2023 11:23:15 |
| Eccentricity: | 0.0055491 |
| inclination: | 97.6665° |
| perigee height: | 601 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 263.0533° |
| argument of perigee: | 329.7595° |
| revolutions per day: | 14.76642029 |
| mean anomaly at epoch: | 30.0417° |
| orbit number at epoch: | 47128 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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