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 46459U 26145.63664231 +.00000000 +00000-0 +72988-3 0 00007
2 46459 97.2308 201.6621 0012409 132.9871 227.2432 15.67013877 01
| Epoch (UTC): | 25 May 2026 15:16:45 |
| Eccentricity: | 0.0012409 |
| inclination: | 97.2308° |
| perigee height: | 359 km |
| apogee height: | 376 km |
| right ascension of ascending node: | 201.6621° |
| argument of perigee: | 132.9871° |
| revolutions per day: | 15.67013877 |
| mean anomaly at epoch: | 227.2432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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