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 25341.97426671 .00023028 00000-0 29194-3 0 9996
2 48274 41.4683 45.6321 0009254 352.4121 7.6575 15.58863749263289
| Epoch (UTC): | 07 December 2025 23:22:56 |
| Eccentricity: | 0.0009254 |
| inclination: | 41.4683° |
| perigee height: | 384 km |
| apogee height: | 397 km |
| right ascension of ascending node: | 45.6321° |
| argument of perigee: | 352.4121° |
| revolutions per day: | 15.58863749 |
| mean anomaly at epoch: | 7.6575° |
| orbit number at epoch: | 26328 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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