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 26106.69521463 +.00000000 +00000-0 -21211-3 0 00000
2 00050 47.2341 352.5935 0113169 191.7215 168.0933 12.20163555 07
| Epoch (UTC): | 16 April 2026 16:41:06 |
| Eccentricity: | 0.0113169 |
| inclination: | 47.2341° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 352.5935° |
| argument of perigee: | 191.7215° |
| revolutions per day: | 12.20163555 |
| mean anomaly at epoch: | 168.0933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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