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 46458U 26145.59970748 +.00000000 +00000-0 +58711-3 0 00002
2 46458 97.2235 195.1666 0012399 222.3217 137.7084 15.58449666 08
| Epoch (UTC): | 25 May 2026 14:23:34 |
| Eccentricity: | 0.0012399 |
| inclination: | 97.2235° |
| perigee height: | 384 km |
| apogee height: | 401 km |
| right ascension of ascending node: | 195.1666° |
| argument of perigee: | 222.3217° |
| revolutions per day: | 15.58449666 |
| mean anomaly at epoch: | 137.7084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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