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 50471U 26145.57310786 +.00000000 +00000-0 -31739-4 0 00003
2 50471 87.9154 10.3759 0002426 100.7188 259.4217 13.17650654 05
| Epoch (UTC): | 25 May 2026 13:45:16 |
| Eccentricity: | 0.0002426 |
| inclination: | 87.9154° |
| perigee height: | 1192 km |
| apogee height: | 1196 km |
| right ascension of ascending node: | 10.3759° |
| argument of perigee: | 100.7188° |
| revolutions per day: | 13.17650654 |
| mean anomaly at epoch: | 259.4217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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