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 67619U 26145.46998756 +.00000000 +00000-0 +78266-3 0 00006
2 67619 43.0002 66.3884 0000791 257.6606 102.4157 15.27587470 00
| Epoch (UTC): | 25 May 2026 11:16:46 |
| Eccentricity: | 0.0000791 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.3884° |
| argument of perigee: | 257.6606° |
| revolutions per day: | 15.27587470 |
| mean anomaly at epoch: | 102.4157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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