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 54148U 26145.41674644 +.00000000 +00000-0 +12444-3 0 00007
2 54148 87.9163 279.0001 0002264 125.7537 234.3807 13.20772565 06
| Epoch (UTC): | 25 May 2026 10:00:06 |
| Eccentricity: | 0.0002264 |
| inclination: | 87.9163° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 279.0001° |
| argument of perigee: | 125.7537° |
| revolutions per day: | 13.20772565 |
| mean anomaly at epoch: | 234.3807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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