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 67373U 26145.46005956 +.00000000 +00000-0 +12675-3 0 00006
2 67373 97.8015 144.3973 0005251 196.0489 164.0563 14.87856365 07
| Epoch (UTC): | 25 May 2026 11:02:29 |
| Eccentricity: | 0.0005251 |
| inclination: | 97.8015° |
| perigee height: | 601 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 144.3973° |
| argument of perigee: | 196.0489° |
| revolutions per day: | 14.87856365 |
| mean anomaly at epoch: | 164.0563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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