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 25345.24140529 .00039326 00000-0 49058-3 0 9994
2 48274 41.4683 25.8033 0008641 18.0340 342.0803 15.59084729263796
| Epoch (UTC): | 11 December 2025 05:47:37 |
| Eccentricity: | 0.0008641 |
| inclination: | 41.4683° |
| perigee height: | 384 km |
| apogee height: | 396 km |
| right ascension of ascending node: | 25.8033° |
| argument of perigee: | 18.0340° |
| revolutions per day: | 15.59084729 |
| mean anomaly at epoch: | 342.0803° |
| orbit number at epoch: | 26379 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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