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 62847U 26145.32755764 +.00000000 +00000-0 +69743-3 0 00009
2 62847 42.9993 16.0017 0001215 281.6691 78.4024 15.27602845 07
| Epoch (UTC): | 25 May 2026 07:51:40 |
| Eccentricity: | 0.0001215 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 16.0017° |
| argument of perigee: | 281.6691° |
| revolutions per day: | 15.27602845 |
| mean anomaly at epoch: | 78.4024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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