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 65599U 26145.43224610 +.00000000 +00000-0 +44621-3 0 00007
2 65599 97.4468 214.0098 0002038 147.4110 212.7243 15.05657873 07
| Epoch (UTC): | 25 May 2026 10:22:26 |
| Eccentricity: | 0.0002038 |
| inclination: | 97.4468° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 214.0098° |
| argument of perigee: | 147.4110° |
| revolutions per day: | 15.05657873 |
| mean anomaly at epoch: | 212.7243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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