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 62425U 26145.57682036 +.00000000 +00000-0 +44105-3 0 00004
2 62425 43.0024 236.2948 0001625 267.4549 92.6117 15.27588531 00
| Epoch (UTC): | 25 May 2026 13:50:37 |
| Eccentricity: | 0.0001625 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.2948° |
| argument of perigee: | 267.4549° |
| revolutions per day: | 15.27588531 |
| mean anomaly at epoch: | 92.6117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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