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 67314U 26145.29170942 +.00000000 +00000-0 +48218-3 0 00002
2 67314 43.0010 252.7047 0000781 259.2703 100.8060 15.27593072 08
| Epoch (UTC): | 25 May 2026 07:00:03 |
| Eccentricity: | 0.0000781 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 252.7047° |
| argument of perigee: | 259.2703° |
| revolutions per day: | 15.27593072 |
| mean anomaly at epoch: | 100.8060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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