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 46808U 26145.63456928 +.00000000 +00000-0 +16871-3 0 00006
2 46808 34.9938 228.4399 0000955 213.4836 146.5812 15.02595721 01
| Epoch (UTC): | 25 May 2026 15:13:46 |
| Eccentricity: | 0.0000955 |
| inclination: | 34.9938° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 228.4399° |
| argument of perigee: | 213.4836° |
| revolutions per day: | 15.02595721 |
| mean anomaly at epoch: | 146.5812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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