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 26073.77149360 +.00000000 +00000-0 +42355-3 0 00005
2 00050 47.2289 94.7858 0112784 93.6360 267.7335 12.20162830 08
| Epoch (UTC): | 14 March 2026 18:30:57 |
| Eccentricity: | 0.0112784 |
| inclination: | 47.2289° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 94.7858° |
| argument of perigee: | 93.6360° |
| revolutions per day: | 12.20162830 |
| mean anomaly at epoch: | 267.7335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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