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 62108U 26145.40286091 +.00000000 +00000-0 +26499-3 0 00001
2 62108 43.0006 132.2949 0001119 269.0892 90.9831 15.27589147 09
| Epoch (UTC): | 25 May 2026 09:40:07 |
| Eccentricity: | 0.0001119 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.2949° |
| argument of perigee: | 269.0892° |
| revolutions per day: | 15.27589147 |
| mean anomaly at epoch: | 90.9831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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