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 67607U 26145.46423392 +.00000000 +00000-0 +47404-3 0 00002
2 67607 97.2853 210.6437 0000189 8.9866 351.1380 15.33458077 04
| Epoch (UTC): | 25 May 2026 11:08:29 |
| Eccentricity: | 0.0000189 |
| inclination: | 97.2853° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.6437° |
| argument of perigee: | 8.9866° |
| revolutions per day: | 15.33458077 |
| mean anomaly at epoch: | 351.1380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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