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 62860U 26145.38785331 +.00000000 +00000-0 +38125-3 0 00003
2 62860 53.1571 133.3121 0001186 93.3894 266.7242 15.30204837 04
| Epoch (UTC): | 25 May 2026 09:18:30 |
| Eccentricity: | 0.0001186 |
| inclination: | 53.1571° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.3121° |
| argument of perigee: | 93.3894° |
| revolutions per day: | 15.30204837 |
| mean anomaly at epoch: | 266.7242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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