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 46172U 26145.52449905 +.00000000 +00000-0 +79418-3 0 00001
2 46172 53.0359 238.1673 0006826 300.9780 59.0569 15.77070147 09
| Epoch (UTC): | 25 May 2026 12:35:16 |
| Eccentricity: | 0.0006826 |
| inclination: | 53.0359° |
| perigee height: | 334 km |
| apogee height: | 343 km |
| right ascension of ascending node: | 238.1673° |
| argument of perigee: | 300.9780° |
| revolutions per day: | 15.77070147 |
| mean anomaly at epoch: | 59.0569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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