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 62456U 26145.54280769 +.00000000 +00000-0 +00000-0 0 00005
2 62456 0.0539 112.9961 0001360 336.4610 141.2288 1.00270114 06
| Epoch (UTC): | 25 May 2026 13:01:38 |
| Eccentricity: | 0.0001360 |
| inclination: | 0.0539° |
| perigee height: | 35781 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 112.9961° |
| argument of perigee: | 336.4610° |
| revolutions per day: | 1.00270114 |
| mean anomaly at epoch: | 141.2288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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