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 25347.15971616 .00001757 00000-0 10078-2 0 9993
2 00012 32.8992 160.8275 1647392 200.0561 152.7069 11.48395513509939
| Epoch (UTC): | 13 December 2025 03:49:59 |
| Eccentricity: | 0.1647392 |
| inclination: | 32.8992° |
| perigee height: | 553 km |
| apogee height: | 3287 km |
| right ascension of ascending node: | 160.8275° |
| argument of perigee: | 200.0561° |
| revolutions per day: | 11.48395513 |
| mean anomaly at epoch: | 152.7069° |
| orbit number at epoch: | 50993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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