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 62525U 26145.44722480 +.00000000 +00000-0 +39939-3 0 00008
2 62525 43.0026 146.7359 0001463 281.7058 78.3630 15.27589914 05
| Epoch (UTC): | 25 May 2026 10:44:00 |
| Eccentricity: | 0.0001463 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.7359° |
| argument of perigee: | 281.7058° |
| revolutions per day: | 15.27589914 |
| mean anomaly at epoch: | 78.3630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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