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 64138U 26145.34049007 +.00000000 +00000-0 +54711-3 0 00001
2 64138 43.0027 5.2021 0002087 267.0918 92.9695 15.27588745 02
| Epoch (UTC): | 25 May 2026 08:10:18 |
| Eccentricity: | 0.0002087 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.2021° |
| argument of perigee: | 267.0918° |
| revolutions per day: | 15.27588745 |
| mean anomaly at epoch: | 92.9695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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