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 67395U 26145.44203213 +.00000000 +00000-0 +87494-4 0 00006
2 67395 97.8037 144.4551 0004827 186.9624 173.1526 14.88025078 05
| Epoch (UTC): | 25 May 2026 10:36:31 |
| Eccentricity: | 0.0004827 |
| inclination: | 97.8037° |
| perigee height: | 601 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 144.4551° |
| argument of perigee: | 186.9624° |
| revolutions per day: | 14.88025078 |
| mean anomaly at epoch: | 173.1526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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