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 67325U 26145.34424780 +.00000000 +00000-0 +56913-3 0 00003
2 67325 42.9990 252.2388 0000417 309.0495 51.0319 15.27594860 06
| Epoch (UTC): | 25 May 2026 08:15:43 |
| Eccentricity: | 0.0000417 |
| inclination: | 42.9990° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 252.2388° |
| argument of perigee: | 309.0495° |
| revolutions per day: | 15.27594860 |
| mean anomaly at epoch: | 51.0319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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