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 65824U 26145.14436962 +.00000000 +00000-0 +58118-3 0 00007
2 65824 53.1575 93.5982 0001210 85.8838 274.2301 15.30200325 03
| Epoch (UTC): | 25 May 2026 03:27:53 |
| Eccentricity: | 0.0001210 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 93.5982° |
| argument of perigee: | 85.8838° |
| revolutions per day: | 15.30200325 |
| mean anomaly at epoch: | 274.2301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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