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 50484U 26145.59506890 +.00000000 +00000-0 +12594-3 0 00008
2 50484 87.8909 25.5620 0002053 88.4882 271.6481 13.11414699 00
| Epoch (UTC): | 25 May 2026 14:16:53 |
| Eccentricity: | 0.0002053 |
| inclination: | 87.8909° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5620° |
| argument of perigee: | 88.4882° |
| revolutions per day: | 13.11414699 |
| mean anomaly at epoch: | 271.6481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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