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 46914U 26145.56704028 +.00000000 +00000-0 +26402-3 0 00004
2 46914 36.9014 207.6799 0004419 91.8355 268.2900 15.24160667 03
| Epoch (UTC): | 25 May 2026 13:36:32 |
| Eccentricity: | 0.0004419 |
| inclination: | 36.9014° |
| perigee height: | 490 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 207.6799° |
| argument of perigee: | 91.8355° |
| revolutions per day: | 15.24160667 |
| mean anomaly at epoch: | 268.2900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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