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 67320U 26145.58023690 +.00000000 +00000-0 +60014-3 0 00006
2 67320 42.9985 251.4344 0001326 277.9230 82.1472 15.27602603 08
| Epoch (UTC): | 25 May 2026 13:55:32 |
| Eccentricity: | 0.0001326 |
| inclination: | 42.9985° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.4344° |
| argument of perigee: | 277.9230° |
| revolutions per day: | 15.27602603 |
| mean anomaly at epoch: | 82.1472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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