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 67369U 26144.94848507 +.00000000 +00000-0 +13942-3 0 00008
2 67369 97.7981 143.7855 0006160 209.8187 150.2679 14.87578195 00
| Epoch (UTC): | 24 May 2026 22:45:49 |
| Eccentricity: | 0.0006160 |
| inclination: | 97.7981° |
| perigee height: | 601 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 143.7855° |
| argument of perigee: | 209.8187° |
| revolutions per day: | 14.87578195 |
| mean anomaly at epoch: | 150.2679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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