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 62984U 26145.36507860 +.00000000 +00000-0 +16788-2 0 00007
2 62984 43.0038 259.0843 0003502 249.8633 110.1858 15.70884405 01
| Epoch (UTC): | 25 May 2026 08:45:42 |
| Eccentricity: | 0.0003502 |
| inclination: | 43.0038° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 259.0843° |
| argument of perigee: | 249.8633° |
| revolutions per day: | 15.70884405 |
| mean anomaly at epoch: | 110.1858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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