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 48274U 21035A 25166.91182113 .00022889 00000-0 29047-3 0 9996
2 48274 41.4647 28.4017 0003757 103.3875 256.7382 15.58879614235955
| Epoch (UTC): | 15 June 2025 21:53:01 |
| Eccentricity: | 0.0003757 |
| inclination: | 41.4647° |
| perigee height: | 388 km |
| apogee height: | 393 km |
| right ascension of ascending node: | 28.4017° |
| argument of perigee: | 103.3875° |
| revolutions per day: | 15.58879614 |
| mean anomaly at epoch: | 256.7382° |
| orbit number at epoch: | 23595 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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