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 50489U 26145.49365735 +.00000000 +00000-0 +92506-4 0 00005
2 50489 87.9167 339.9731 0001952 79.5100 280.6252 13.18687684 07
| Epoch (UTC): | 25 May 2026 11:50:51 |
| Eccentricity: | 0.0001952 |
| inclination: | 87.9167° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9731° |
| argument of perigee: | 79.5100° |
| revolutions per day: | 13.18687684 |
| mean anomaly at epoch: | 280.6252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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