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 46155U 26145.58335647 +.00000000 +00000-0 +10260-2 0 00004
2 46155 53.0137 202.4909 0008721 15.0310 168.6051 15.83590008 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0008721 |
| inclination: | 53.0137° |
| perigee height: | 314 km |
| apogee height: | 326 km |
| right ascension of ascending node: | 202.4909° |
| argument of perigee: | 15.0310° |
| revolutions per day: | 15.83590008 |
| mean anomaly at epoch: | 168.6051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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