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 66429U 26145.45828385 +.00000000 +00000-0 +42688-3 0 00002
2 66429 42.9999 200.6631 0001520 272.5845 87.4832 15.27584943 00
| Epoch (UTC): | 25 May 2026 10:59:55 |
| Eccentricity: | 0.0001520 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.6631° |
| argument of perigee: | 272.5845° |
| revolutions per day: | 15.27584943 |
| mean anomaly at epoch: | 87.4832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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