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 45856U 26145.64589435 +.00000000 +00000-0 +72006-4 0 00002
2 45856 97.7756 206.3510 0011818 139.8751 220.3334 14.76842086 04
| Epoch (UTC): | 25 May 2026 15:30:05 |
| Eccentricity: | 0.0011818 |
| inclination: | 97.7756° |
| perigee height: | 631 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 206.3510° |
| argument of perigee: | 139.8751° |
| revolutions per day: | 14.76842086 |
| mean anomaly at epoch: | 220.3334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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