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 50470U 26145.34361227 +.00000000 +00000-0 -63726-4 0 00004
2 50470 87.9153 10.4119 0001690 90.8092 269.3233 13.17650738 00
| Epoch (UTC): | 25 May 2026 08:14:48 |
| Eccentricity: | 0.0001690 |
| inclination: | 87.9153° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4119° |
| argument of perigee: | 90.8092° |
| revolutions per day: | 13.17650738 |
| mean anomaly at epoch: | 269.3233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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