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 25167.03995113 .00023293 00000-0 29544-3 0 9994
2 48274 41.4648 27.6240 0003751 104.8581 255.2673 15.58885725235978
| Epoch (UTC): | 16 June 2025 00:57:31 |
| Eccentricity: | 0.0003751 |
| inclination: | 41.4648° |
| perigee height: | 388 km |
| apogee height: | 393 km |
| right ascension of ascending node: | 27.6240° |
| argument of perigee: | 104.8581° |
| revolutions per day: | 15.58885725 |
| mean anomaly at epoch: | 255.2673° |
| orbit number at epoch: | 23597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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