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 50834U 26145.34156961 +.00000000 +00000-0 -12884-4 0 00004
2 50834 53.2123 195.0220 0000986 88.9808 271.1298 15.08835474 06
| Epoch (UTC): | 25 May 2026 08:11:51 |
| Eccentricity: | 0.0000986 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 195.0220° |
| argument of perigee: | 88.9808° |
| revolutions per day: | 15.08835474 |
| mean anomaly at epoch: | 271.1298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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