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 67379U 26145.58335647 +.00000000 +00000-0 -42653-2 0 00007
2 67379 97.8042 144.5007 0001040 217.0099 121.9911 14.86298565 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001040 |
| inclination: | 97.8042° |
| perigee height: | 609 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 144.5007° |
| argument of perigee: | 217.0099° |
| revolutions per day: | 14.86298565 |
| mean anomaly at epoch: | 121.9911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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