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 62050U 26145.57374199 +.00000000 +00000-0 +52669-3 0 00000
2 62050 43.0034 189.0816 0001868 269.8157 90.2481 15.27591736 03
| Epoch (UTC): | 25 May 2026 13:46:11 |
| Eccentricity: | 0.0001868 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.0816° |
| argument of perigee: | 269.8157° |
| revolutions per day: | 15.27591736 |
| mean anomaly at epoch: | 90.2481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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