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 67237U 26145.41572395 +.00000000 +00000-0 +75107-4 0 00006
2 67237 50.0057 197.2707 0000941 247.2600 112.8173 13.29324017 07
| Epoch (UTC): | 25 May 2026 09:58:38 |
| Eccentricity: | 0.0000941 |
| inclination: | 50.0057° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 197.2707° |
| argument of perigee: | 247.2600° |
| revolutions per day: | 13.29324017 |
| mean anomaly at epoch: | 112.8173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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