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 25342.61491639 .00028320 00000-0 35728-3 0 9994
2 48274 41.4682 41.7451 0009131 357.4459 2.6332 15.58905517263389
| Epoch (UTC): | 08 December 2025 14:45:28 |
| Eccentricity: | 0.0009131 |
| inclination: | 41.4682° |
| perigee height: | 384 km |
| apogee height: | 397 km |
| right ascension of ascending node: | 41.7451° |
| argument of perigee: | 357.4459° |
| revolutions per day: | 15.58905517 |
| mean anomaly at epoch: | 2.6332° |
| orbit number at epoch: | 26338 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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