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 62046U 26145.53487373 +.00000000 +00000-0 +29367-3 0 00009
2 62046 42.9996 181.8634 0001440 267.3190 92.7497 15.27580332 01
| Epoch (UTC): | 25 May 2026 12:50:13 |
| Eccentricity: | 0.0001440 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 181.8634° |
| argument of perigee: | 267.3190° |
| revolutions per day: | 15.27580332 |
| mean anomaly at epoch: | 92.7497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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