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 50488U 26145.36448110 +.00000000 +00000-0 +36512-3 0 00003
2 50488 87.8914 25.5948 0001935 90.2907 269.8443 13.11414462 05
| Epoch (UTC): | 25 May 2026 08:44:51 |
| Eccentricity: | 0.0001935 |
| inclination: | 87.8914° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5948° |
| argument of perigee: | 90.2907° |
| revolutions per day: | 13.11414462 |
| mean anomaly at epoch: | 269.8443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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