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 67302U 26145.74098975 +.00000000 +00000-0 +00000-0 0 00008
2 67302 3.3426 95.6460 0002971 333.1791 155.1089 1.00275792 06
| Epoch (UTC): | 25 May 2026 17:47:01 |
| Eccentricity: | 0.0002971 |
| inclination: | 3.3426° |
| perigee height: | 35773 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 95.6460° |
| argument of perigee: | 333.1791° |
| revolutions per day: | 1.00275792 |
| mean anomaly at epoch: | 155.1089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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