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 62529U 26145.36384824 +.00000000 +00000-0 +44412-3 0 00001
2 62529 42.9989 146.9629 0001498 274.1907 85.8773 15.27588764 07
| Epoch (UTC): | 25 May 2026 08:43:56 |
| Eccentricity: | 0.0001498 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.9629° |
| argument of perigee: | 274.1907° |
| revolutions per day: | 15.27588764 |
| mean anomaly at epoch: | 85.8773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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