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 41457U 26106.75367485 +.00000000 +00000-0 +11853-3 0 00005
2 41457 98.2476 119.7860 0001672 78.6756 281.4631 14.59486797 01
| Epoch (UTC): | 16 April 2026 18:05:17 |
| Eccentricity: | 0.0001672 |
| inclination: | 98.2476° |
| perigee height: | 694 km |
| apogee height: | 696 km |
| right ascension of ascending node: | 119.7860° |
| argument of perigee: | 78.6756° |
| revolutions per day: | 14.59486797 |
| mean anomaly at epoch: | 281.4631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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