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 00012U 59001B 25201.54165482 .00000944 00000-0 55504-3 0 9992
2 00012 32.8995 313.6002 1647392 149.4480 221.3379 11.47800895493194
| Epoch (UTC): | 20 July 2025 12:59:58 |
| Eccentricity: | 0.1647392 |
| inclination: | 32.8995° |
| perigee height: | 556 km |
| apogee height: | 3291 km |
| right ascension of ascending node: | 313.6002° |
| argument of perigee: | 149.4480° |
| revolutions per day: | 11.47800895 |
| mean anomaly at epoch: | 221.3379° |
| orbit number at epoch: | 49319 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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