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 67044U 26145.51848662 +.00000000 +00000-0 +64946-3 0 00004
2 67044 42.9977 323.8080 0000430 272.4816 87.5986 15.27589488 02
| Epoch (UTC): | 25 May 2026 12:26:37 |
| Eccentricity: | 0.0000430 |
| inclination: | 42.9977° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 323.8080° |
| argument of perigee: | 272.4816° |
| revolutions per day: | 15.27589488 |
| mean anomaly at epoch: | 87.5986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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