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 62045U 26145.58242135 +.00000000 +00000-0 +56517-3 0 00005
2 62045 42.9992 182.2175 0001633 274.8740 85.1926 15.27593230 03
| Epoch (UTC): | 25 May 2026 13:58:41 |
| Eccentricity: | 0.0001633 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.2175° |
| argument of perigee: | 274.8740° |
| revolutions per day: | 15.27593230 |
| mean anomaly at epoch: | 85.1926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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