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 46340U 26144.75629286 +.00000000 +00000-0 +81249-3 0 00009
2 46340 53.0175 315.0814 0003996 236.7270 123.3367 15.78028311 07
| Epoch (UTC): | 24 May 2026 18:09:03 |
| Eccentricity: | 0.0003996 |
| inclination: | 53.0175° |
| perigee height: | 333 km |
| apogee height: | 339 km |
| right ascension of ascending node: | 315.0814° |
| argument of perigee: | 236.7270° |
| revolutions per day: | 15.78028311 |
| mean anomaly at epoch: | 123.3367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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