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 39434U 13066U 23083.43033709 .00246661 00000-0 62030-2 0 9992
2 39434 97.4253 153.3799 0016567 167.2737 192.8930 15.38842449512244
| Epoch (UTC): | 24 March 2023 10:19:41 |
| Eccentricity: | 0.0016567 |
| inclination: | 97.4253° |
| perigee height: | 438 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 153.3799° |
| argument of perigee: | 167.2737° |
| revolutions per day: | 15.38842449 |
| mean anomaly at epoch: | 192.8930° |
| orbit number at epoch: | 51224 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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