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 67570U 26145.59222551 +.00000000 +00000-0 +86650-3 0 00005
2 67570 97.2857 205.9772 0000245 152.3826 207.7429 15.33467558 03
| Epoch (UTC): | 25 May 2026 14:12:48 |
| Eccentricity: | 0.0000245 |
| inclination: | 97.2857° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.9772° |
| argument of perigee: | 152.3826° |
| revolutions per day: | 15.33467558 |
| mean anomaly at epoch: | 207.7429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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