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 65241U 26145.54951880 +.00000000 +00000-0 -27125-3 0 00000
2 65241 97.4477 188.3530 0002426 90.3377 269.8128 15.05653196 06
| Epoch (UTC): | 25 May 2026 13:11:18 |
| Eccentricity: | 0.0002426 |
| inclination: | 97.4477° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.3530° |
| argument of perigee: | 90.3377° |
| revolutions per day: | 15.05653196 |
| mean anomaly at epoch: | 269.8128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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