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 is defined by the following mean orbital elements,
1 00059U 26025.02152134 +.00000000 +00000-0 +10340-3 0 00001
2 00059 28.2478 139.1630 0188751 193.8751 165.6553 13.53159119 03
| Epoch (UTC): | 25 January 2026 00:30:59 |
| Eccentricity: | 0.0188751 |
| inclination: | 28.2478° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 139.1630° |
| argument of perigee: | 193.8751° |
| revolutions per day: | 13.53159119 |
| mean anomaly at epoch: | 165.6553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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