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 46506U 26145.44027644 +.00000000 +00000-0 +39582-3 0 00003
2 46506 97.8749 144.7093 0006923 91.3225 268.8810 15.34005001 09
| Epoch (UTC): | 25 May 2026 10:33:59 |
| Eccentricity: | 0.0006923 |
| inclination: | 97.8749° |
| perigee height: | 459 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 144.7093° |
| argument of perigee: | 91.3225° |
| revolutions per day: | 15.34005001 |
| mean anomaly at epoch: | 268.8810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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