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 46905U 26145.67268602 +.00000000 +00000-0 +26854-3 0 00000
2 46905 36.9000 357.9673 0012036 331.2199 28.7878 15.01467417 00
| Epoch (UTC): | 25 May 2026 16:08:40 |
| Eccentricity: | 0.0012036 |
| inclination: | 36.9000° |
| perigee height: | 554 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 357.9673° |
| argument of perigee: | 331.2199° |
| revolutions per day: | 15.01467417 |
| mean anomaly at epoch: | 28.7878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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