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 62109U 26145.32334870 +.00000000 +00000-0 +54025-3 0 00008
2 62109 42.9988 132.5569 0001328 273.7017 86.3682 15.27580415 03
| Epoch (UTC): | 25 May 2026 07:45:37 |
| Eccentricity: | 0.0001328 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.5569° |
| argument of perigee: | 273.7017° |
| revolutions per day: | 15.27580415 |
| mean anomaly at epoch: | 86.3682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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