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 46129U 26145.53113350 +.00000000 +00000-0 +68670-3 0 00004
2 46129 53.0433 240.3625 0004534 348.7076 11.3839 15.71604149 08
| Epoch (UTC): | 25 May 2026 12:44:49 |
| Eccentricity: | 0.0004534 |
| inclination: | 53.0433° |
| perigee height: | 351 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 240.3625° |
| argument of perigee: | 348.7076° |
| revolutions per day: | 15.71604149 |
| mean anomaly at epoch: | 11.3839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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