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 25163.00357684 .00019785 00000-0 25389-3 0 9996
2 48274 41.4651 52.1156 0004051 63.3767 296.7486 15.58653040235346
| Epoch (UTC): | 12 June 2025 00:05:09 |
| Eccentricity: | 0.0004051 |
| inclination: | 41.4651° |
| perigee height: | 389 km |
| apogee height: | 394 km |
| right ascension of ascending node: | 52.1156° |
| argument of perigee: | 63.3767° |
| revolutions per day: | 15.58653040 |
| mean anomaly at epoch: | 296.7486° |
| orbit number at epoch: | 23534 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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