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 46715U 26145.44008801 +.00000000 +00000-0 +67215-3 0 00003
2 46715 53.0438 198.1495 0003433 21.6520 338.4644 15.76600620 09
| Epoch (UTC): | 25 May 2026 10:33:43 |
| Eccentricity: | 0.0003433 |
| inclination: | 53.0438° |
| perigee height: | 338 km |
| apogee height: | 342 km |
| right ascension of ascending node: | 198.1495° |
| argument of perigee: | 21.6520° |
| revolutions per day: | 15.76600620 |
| mean anomaly at epoch: | 338.4644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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