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 67374U 26145.22942295 +.00000000 +00000-0 +75219-4 0 00001
2 67374 97.7997 144.2113 0003463 183.7033 176.4158 14.87996944 07
| Epoch (UTC): | 25 May 2026 05:30:22 |
| Eccentricity: | 0.0003463 |
| inclination: | 97.7997° |
| perigee height: | 602 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 144.2113° |
| argument of perigee: | 183.7033° |
| revolutions per day: | 14.87996944 |
| mean anomaly at epoch: | 176.4158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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