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 67966U 26145.46977344 +.00000000 +00000-0 +53892-3 0 00009
2 67966 97.2843 155.4578 0001043 98.3220 261.8141 15.33459864 07
| Epoch (UTC): | 25 May 2026 11:16:28 |
| Eccentricity: | 0.0001043 |
| inclination: | 97.2843° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4578° |
| argument of perigee: | 98.3220° |
| revolutions per day: | 15.33459864 |
| mean anomaly at epoch: | 261.8141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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