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 53667U 26145.66668980 +.00000000 +00000-0 -12688-1 0 00004
2 53667 97.6041 28.7289 0002036 68.2075 143.5782 15.32774672 05
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0002036 |
| inclination: | 97.6041° |
| perigee height: | 466 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 28.7289° |
| argument of perigee: | 68.2075° |
| revolutions per day: | 15.32774672 |
| mean anomaly at epoch: | 143.5782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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