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 67628U 26145.50581520 +.00000000 +00000-0 +31094-3 0 00006
2 67628 43.0002 65.7738 0000755 196.3858 163.6970 15.27590982 03
| Epoch (UTC): | 25 May 2026 12:08:22 |
| Eccentricity: | 0.0000755 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 65.7738° |
| argument of perigee: | 196.3858° |
| revolutions per day: | 15.27590982 |
| mean anomaly at epoch: | 163.6970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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