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 25136.49725264 .00028146 00000-0 31583-3 0 9996
2 48274 41.4638 213.2077 0006338 280.9374 79.0752 15.61990096231202
| Epoch (UTC): | 16 May 2025 11:56:02 |
| Eccentricity: | 0.0006338 |
| inclination: | 41.4638° |
| perigee height: | 377 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 213.2077° |
| argument of perigee: | 280.9374° |
| revolutions per day: | 15.61990096 |
| mean anomaly at epoch: | 79.0752° |
| orbit number at epoch: | 23120 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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