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 46713U 26145.58335647 +.00000000 +00000-0 +10743-2 0 00000
2 46713 53.0354 177.0265 0009167 3.4474 168.5656 15.92356174 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0009167 |
| inclination: | 53.0354° |
| perigee height: | 290 km |
| apogee height: | 302 km |
| right ascension of ascending node: | 177.0265° |
| argument of perigee: | 3.4474° |
| revolutions per day: | 15.92356174 |
| mean anomaly at epoch: | 168.5656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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