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 50841U 26145.39676804 +.00000000 +00000-0 -10068-5 0 00003
2 50841 53.2120 194.7701 0000595 60.3615 299.7436 15.08835015 08
| Epoch (UTC): | 25 May 2026 09:31:20 |
| Eccentricity: | 0.0000595 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 194.7701° |
| argument of perigee: | 60.3615° |
| revolutions per day: | 15.08835015 |
| mean anomaly at epoch: | 299.7436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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