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 53867U 26145.66668980 +.00000000 +00000-0 -23255-1 0 00008
2 53867 53.2168 283.6059 0000993 82.0206 288.9404 15.32908975 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000993 |
| inclination: | 53.2168° |
| perigee height: | 466 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 283.6059° |
| argument of perigee: | 82.0206° |
| revolutions per day: | 15.32908975 |
| mean anomaly at epoch: | 288.9404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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