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 46709U 26145.49559572 +.00000000 +00000-0 +10422-2 0 00004
2 46709 53.0417 221.2860 0006125 351.5275 8.5633 15.60357714 05
| Epoch (UTC): | 25 May 2026 11:53:39 |
| Eccentricity: | 0.0006125 |
| inclination: | 53.0417° |
| perigee height: | 382 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 221.2860° |
| argument of perigee: | 351.5275° |
| revolutions per day: | 15.60357714 |
| mean anomaly at epoch: | 8.5633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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