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 50849U 26145.50716781 +.00000000 +00000-0 -79934-4 0 00009
2 50849 53.2100 194.2748 0001270 90.6620 269.4518 15.08844943 08
| Epoch (UTC): | 25 May 2026 12:10:19 |
| Eccentricity: | 0.0001270 |
| inclination: | 53.2100° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 194.2748° |
| argument of perigee: | 90.6620° |
| revolutions per day: | 15.08844943 |
| mean anomaly at epoch: | 269.4518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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