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 50492U 26145.26433993 +.00000000 +00000-0 +47127-4 0 00005
2 50492 87.9160 340.0204 0002004 93.7801 266.3560 13.18688011 05
| Epoch (UTC): | 25 May 2026 06:20:38 |
| Eccentricity: | 0.0002004 |
| inclination: | 87.9160° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0204° |
| argument of perigee: | 93.7801° |
| revolutions per day: | 13.18688011 |
| mean anomaly at epoch: | 266.3560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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