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 00050U 26159.76679882 +.00000000 +00000-0 -87204-4 0 00000
2 00050 47.2280 187.8643 0113437 349.4208 10.4200 12.20165880 06
| Epoch (UTC): | 08 June 2026 18:24:11 |
| Eccentricity: | 0.0113437 |
| inclination: | 47.2280° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 187.8643° |
| argument of perigee: | 349.4208° |
| revolutions per day: | 12.20165880 |
| mean anomaly at epoch: | 10.4200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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