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 25140.45409239 .00000587 00000-0 33047-3 0 9996
2 00012 32.8970 168.5742 1649338 186.3781 171.3063 11.47728877486174
| Epoch (UTC): | 20 May 2025 10:53:53 |
| Eccentricity: | 0.1649338 |
| inclination: | 32.8970° |
| perigee height: | 554 km |
| apogee height: | 3293 km |
| right ascension of ascending node: | 168.5742° |
| argument of perigee: | 186.3781° |
| revolutions per day: | 11.47728877 |
| mean anomaly at epoch: | 171.3063° |
| orbit number at epoch: | 48617 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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