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 25193.56496263 .00010039 00000-0 13433-3 0 9997
2 48274 41.4634 226.6836 0013748 271.0550 88.8712 15.57900588240115
| Epoch (UTC): | 12 July 2025 13:33:32 |
| Eccentricity: | 0.0013748 |
| inclination: | 41.4634° |
| perigee height: | 384 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 226.6836° |
| argument of perigee: | 271.0550° |
| revolutions per day: | 15.57900588 |
| mean anomaly at epoch: | 88.8712° |
| orbit number at epoch: | 24011 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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