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 50843U 26142.54747891 +.00000000 +00000-0 +61579-3 0 00004
2 50843 53.2069 162.4605 0008262 10.0713 350.0495 16.27218699 08
| Epoch (UTC): | 22 May 2026 13:08:22 |
| Eccentricity: | 0.0008262 |
| inclination: | 53.2069° |
| perigee height: | 195 km |
| apogee height: | 205 km |
| right ascension of ascending node: | 162.4605° |
| argument of perigee: | 10.0713° |
| revolutions per day: | 16.27218699 |
| mean anomaly at epoch: | 350.0495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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