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 38767U 26145.30346863 +.00000000 +00000-0 +10399-2 0 00009
2 38767 64.6275 109.7205 0018323 214.3328 145.6645 15.81436502 03
| Epoch (UTC): | 25 May 2026 07:16:59 |
| Eccentricity: | 0.0018323 |
| inclination: | 64.6275° |
| perigee height: | 314 km |
| apogee height: | 339 km |
| right ascension of ascending node: | 109.7205° |
| argument of perigee: | 214.3328° |
| revolutions per day: | 15.81436502 |
| mean anomaly at epoch: | 145.6645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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