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 54668U 26145.51145822 +.00000000 +00000-0 +77878-5 0 00000
2 54668 87.9261 248.4834 0001902 100.6056 259.5293 13.21825357 09
| Epoch (UTC): | 25 May 2026 12:16:29 |
| Eccentricity: | 0.0001902 |
| inclination: | 87.9261° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4834° |
| argument of perigee: | 100.6056° |
| revolutions per day: | 13.21825357 |
| mean anomaly at epoch: | 259.5293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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