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 65236U 26145.55783933 +.00000000 +00000-0 +19501-3 0 00005
2 65236 97.4452 188.3397 0002168 122.0367 238.1072 15.05655437 06
| Epoch (UTC): | 25 May 2026 13:23:17 |
| Eccentricity: | 0.0002168 |
| inclination: | 97.4452° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.3397° |
| argument of perigee: | 122.0367° |
| revolutions per day: | 15.05655437 |
| mean anomaly at epoch: | 238.1072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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