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 46807U 26145.65678816 +.00000000 +00000-0 +16810-3 0 00002
2 46807 34.9933 228.5456 0000670 257.8274 102.2359 15.02578815 02
| Epoch (UTC): | 25 May 2026 15:45:46 |
| Eccentricity: | 0.0000670 |
| inclination: | 34.9933° |
| perigee height: | 558 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 228.5456° |
| argument of perigee: | 257.8274° |
| revolutions per day: | 15.02578815 |
| mean anomaly at epoch: | 102.2359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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