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 62062U 26145.15894891 +.00000000 +00000-0 +14453-2 0 00001
2 62062 53.1571 54.3071 0001014 83.7108 276.4026 15.69768665 09
| Epoch (UTC): | 25 May 2026 03:48:53 |
| Eccentricity: | 0.0001014 |
| inclination: | 53.1571° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 54.3071° |
| argument of perigee: | 83.7108° |
| revolutions per day: | 15.69768665 |
| mean anomaly at epoch: | 276.4026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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