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 43773U 18099R 25138.85043023 .00004957 00000-0 31804-3 0 9999
2 43773 97.4494 187.8835 0009482 264.6165 95.3982 15.08893945352947
| Epoch (UTC): | 18 May 2025 20:24:37 |
| Eccentricity: | 0.0009482 |
| inclination: | 97.4494° |
| perigee height: | 533 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 187.8835° |
| argument of perigee: | 264.6165° |
| revolutions per day: | 15.08893945 |
| mean anomaly at epoch: | 95.3982° |
| orbit number at epoch: | 35294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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