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 67571U 26145.63027778 +.00000000 +00000-0 +65336-3 0 00003
2 67571 97.2850 205.9246 0000942 259.0829 101.0308 15.33463251 03
| Epoch (UTC): | 25 May 2026 15:07:36 |
| Eccentricity: | 0.0000942 |
| inclination: | 97.2850° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.9246° |
| argument of perigee: | 259.0829° |
| revolutions per day: | 15.33463251 |
| mean anomaly at epoch: | 101.0308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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