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 67364U 26144.95366558 +.00000000 +00000-0 +16537-3 0 00008
2 67364 97.8060 143.8967 0008039 196.3107 163.7852 14.87607705 00
| Epoch (UTC): | 24 May 2026 22:53:16 |
| Eccentricity: | 0.0008039 |
| inclination: | 97.8060° |
| perigee height: | 600 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 143.8967° |
| argument of perigee: | 196.3107° |
| revolutions per day: | 14.87607705 |
| mean anomaly at epoch: | 163.7852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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