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 25134.45266700 .00000637 00000-0 36778-3 0 9993
2 00012 32.8952 189.6999 1649356 154.6251 214.5480 11.47722137485481
| Epoch (UTC): | 14 May 2025 10:51:50 |
| Eccentricity: | 0.1649356 |
| inclination: | 32.8952° |
| perigee height: | 554 km |
| apogee height: | 3293 km |
| right ascension of ascending node: | 189.6999° |
| argument of perigee: | 154.6251° |
| revolutions per day: | 11.47722137 |
| mean anomaly at epoch: | 214.5480° |
| orbit number at epoch: | 48548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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