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 50496U 26145.47848250 +.00000000 +00000-0 +73916-4 0 00003
2 50496 87.9166 339.9763 0002150 82.2588 277.8788 13.18685396 01
| Epoch (UTC): | 25 May 2026 11:29:00 |
| Eccentricity: | 0.0002150 |
| inclination: | 87.9166° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9763° |
| argument of perigee: | 82.2588° |
| revolutions per day: | 13.18685396 |
| mean anomaly at epoch: | 277.8788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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