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 62145U 26145.54978399 +.00000000 +00000-0 +70680-3 0 00007
2 62145 43.0005 84.1337 0000965 261.6679 98.4064 15.27592001 08
| Epoch (UTC): | 25 May 2026 13:11:41 |
| Eccentricity: | 0.0000965 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 84.1337° |
| argument of perigee: | 261.6679° |
| revolutions per day: | 15.27592001 |
| mean anomaly at epoch: | 98.4064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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