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 48226U 26145.37854808 +.00000000 +00000-0 -57061-4 0 00000
2 48226 87.8949 294.2436 0001753 106.7998 253.3324 13.14504001 06
| Epoch (UTC): | 25 May 2026 09:05:06 |
| Eccentricity: | 0.0001753 |
| inclination: | 87.8949° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2436° |
| argument of perigee: | 106.7998° |
| revolutions per day: | 13.14504001 |
| mean anomaly at epoch: | 253.3324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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