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 65997U 26145.30226497 +.00000000 +00000-0 +43888-4 0 00005
2 65997 49.9970 257.7915 0000926 153.5450 206.5469 13.29327240 07
| Epoch (UTC): | 25 May 2026 07:15:15 |
| Eccentricity: | 0.0000926 |
| inclination: | 49.9970° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 257.7915° |
| argument of perigee: | 153.5450° |
| revolutions per day: | 13.29327240 |
| mean anomaly at epoch: | 206.5469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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