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 65240U 26145.36400110 +.00000000 +00000-0 +33573-3 0 00007
2 65240 97.4453 188.1392 0001805 133.9221 226.2155 15.05654010 08
| Epoch (UTC): | 25 May 2026 08:44:09 |
| Eccentricity: | 0.0001805 |
| inclination: | 97.4453° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.1392° |
| argument of perigee: | 133.9221° |
| revolutions per day: | 15.05654010 |
| mean anomaly at epoch: | 226.2155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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