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 26133.39458280 +.00000000 +00000-0 -29182-3 0 00008
2 00050 47.2317 269.7212 0113531 271.0310 87.7474 12.20164652 04
| Epoch (UTC): | 13 May 2026 09:28:11 |
| Eccentricity: | 0.0113531 |
| inclination: | 47.2317° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 269.7212° |
| argument of perigee: | 271.0310° |
| revolutions per day: | 12.20164652 |
| mean anomaly at epoch: | 87.7474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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