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 67706U 26145.57747557 +.00000000 +00000-0 +84468-3 0 00007
2 67706 97.2846 257.1521 0000818 100.3449 259.7886 15.33457145 08
| Epoch (UTC): | 25 May 2026 13:51:33 |
| Eccentricity: | 0.0000818 |
| inclination: | 97.2846° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1521° |
| argument of perigee: | 100.3449° |
| revolutions per day: | 15.33457145 |
| mean anomaly at epoch: | 259.7886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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