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 67306U 26145.63662772 +.00000000 +00000-0 +10965-2 0 00005
2 67306 42.9990 251.0010 0001582 266.1155 93.9516 15.27604629 03
| Epoch (UTC): | 25 May 2026 15:16:44 |
| Eccentricity: | 0.0001582 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.0010° |
| argument of perigee: | 266.1155° |
| revolutions per day: | 15.27604629 |
| mean anomaly at epoch: | 93.9516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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