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 25344.15240991 .00032718 00000-0 41039-3 0 9996
2 48274 41.4682 32.4132 0008862 9.3921 350.7081 15.59004040263626
| Epoch (UTC): | 10 December 2025 03:39:28 |
| Eccentricity: | 0.0008862 |
| inclination: | 41.4682° |
| perigee height: | 384 km |
| apogee height: | 396 km |
| right ascension of ascending node: | 32.4132° |
| argument of perigee: | 9.3921° |
| revolutions per day: | 15.59004040 |
| mean anomaly at epoch: | 350.7081° |
| orbit number at epoch: | 26362 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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