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 00046U 26140.48254419 +.00000000 +00000-0 +59041-4 0 00006
2 00046 66.6880 303.7767 0200487 312.7069 45.7307 14.54841292 04
| Epoch (UTC): | 20 May 2026 11:34:51 |
| Eccentricity: | 0.0200487 |
| inclination: | 66.6880° |
| perigee height: | 568 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 303.7767° |
| argument of perigee: | 312.7069° |
| revolutions per day: | 14.54841292 |
| mean anomaly at epoch: | 45.7307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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