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 40024U 14033Q 23081.39770887 .00009179 00000-0 85223-3 0 9993
2 40024 98.0193 34.4779 0010079 200.9737 159.1070 14.94595236475963
| Epoch (UTC): | 22 March 2023 09:32:42 |
| Eccentricity: | 0.0010079 |
| inclination: | 98.0193° |
| perigee height: | 576 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 34.4779° |
| argument of perigee: | 200.9737° |
| revolutions per day: | 14.94595236 |
| mean anomaly at epoch: | 159.1070° |
| orbit number at epoch: | 47596 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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