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 41789U 26099.05904417 +.00000000 +00000-0 +18416-3 0 00001
2 41789 97.8032 105.4910 0027215 51.0257 309.3368 14.69193563 06
| Epoch (UTC): | 09 April 2026 01:25:01 |
| Eccentricity: | 0.0027215 |
| inclination: | 97.8032° |
| perigee height: | 644 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 105.4910° |
| argument of perigee: | 51.0257° |
| revolutions per day: | 14.69193563 |
| mean anomaly at epoch: | 309.3368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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