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 34223U 02024H 25131.59372537 .00000477 00000-0 30270-3 0 9998
2 34223 99.1046 177.4914 0129666 34.3357 326.6106 14.04614260154959
| Epoch (UTC): | 11 May 2025 14:14:57 |
| Eccentricity: | 0.0129666 |
| inclination: | 99.1046° |
| perigee height: | 784 km |
| apogee height: | 972 km |
| right ascension of ascending node: | 177.4914° |
| argument of perigee: | 34.3357° |
| revolutions per day: | 14.04614260 |
| mean anomaly at epoch: | 326.6106° |
| orbit number at epoch: | 15495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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