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 65663U 26145.12167741 +.00000000 +00000-0 +13765-3 0 00001
2 65663 97.4477 189.0522 0002231 118.7212 241.4240 15.05655376 03
| Epoch (UTC): | 25 May 2026 02:55:12 |
| Eccentricity: | 0.0002231 |
| inclination: | 97.4477° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.0522° |
| argument of perigee: | 118.7212° |
| revolutions per day: | 15.05655376 |
| mean anomaly at epoch: | 241.4240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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