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 02142U 66031A 23083.09681538 .00000775 00000-0 28092-3 0 9994
2 02142 35.0465 303.6893 0006585 31.2390 328.8688 14.34030650981409
| Epoch (UTC): | 24 March 2023 02:19:24 |
| Eccentricity: | 0.0006585 |
| inclination: | 35.0465° |
| perigee height: | 773 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 303.6893° |
| argument of perigee: | 31.2390° |
| revolutions per day: | 14.34030650 |
| mean anomaly at epoch: | 328.8688° |
| orbit number at epoch: | 98140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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