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 38867U 26145.43064675 +.00000000 +00000-0 +00000-0 0 00008
2 38867 0.0112 313.3224 0000359 192.4297 199.2991 1.00275735 07
| Epoch (UTC): | 25 May 2026 10:20:07 |
| Eccentricity: | 0.0000359 |
| inclination: | 0.0112° |
| perigee height: | 35784 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 313.3224° |
| argument of perigee: | 192.4297° |
| revolutions per day: | 1.00275735 |
| mean anomaly at epoch: | 199.2991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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