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 25187.28238512 .00020645 00000-0 27281-3 0 9990
2 48274 41.4649 264.7513 0013558 229.8701 130.0949 15.57755571239136
| Epoch (UTC): | 06 July 2025 06:46:38 |
| Eccentricity: | 0.0013558 |
| inclination: | 41.4649° |
| perigee height: | 385 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 264.7513° |
| argument of perigee: | 229.8701° |
| revolutions per day: | 15.57755571 |
| mean anomaly at epoch: | 130.0949° |
| orbit number at epoch: | 23913 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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