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 67368U 26145.25287238 +.00000000 +00000-0 +38174-3 0 00004
2 67368 97.8043 144.2573 0007361 195.4814 164.6179 14.88325181 03
| Epoch (UTC): | 25 May 2026 06:04:08 |
| Eccentricity: | 0.0007361 |
| inclination: | 97.8043° |
| perigee height: | 598 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 144.2573° |
| argument of perigee: | 195.4814° |
| revolutions per day: | 14.88325181 |
| mean anomaly at epoch: | 164.6179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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