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 67219U 26145.54654346 +.00000000 +00000-0 +57000-3 0 00008
2 67219 45.0014 203.1999 0005075 18.8296 341.2767 15.09275170 02
| Epoch (UTC): | 25 May 2026 13:07:01 |
| Eccentricity: | 0.0005075 |
| inclination: | 45.0014° |
| perigee height: | 535 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 203.1999° |
| argument of perigee: | 18.8296° |
| revolutions per day: | 15.09275170 |
| mean anomaly at epoch: | 341.2767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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