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 46357U 26145.58412663 +.00000000 +00000-0 +21813-3 0 00009
2 46357 53.0369 315.6146 0000929 276.9880 83.1033 15.76235446 00
| Epoch (UTC): | 25 May 2026 14:01:08 |
| Eccentricity: | 0.0000929 |
| inclination: | 53.0369° |
| perigee height: | 340 km |
| apogee height: | 342 km |
| right ascension of ascending node: | 315.6146° |
| argument of perigee: | 276.9880° |
| revolutions per day: | 15.76235446 |
| mean anomaly at epoch: | 83.1033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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