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 48221U 26145.66700876 +.00000000 +00000-0 -46315-3 0 00001
2 48221 87.8932 294.2064 0001830 106.0852 254.0479 13.14501420 09
| Epoch (UTC): | 25 May 2026 16:00:29 |
| Eccentricity: | 0.0001830 |
| inclination: | 87.8932° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2064° |
| argument of perigee: | 106.0852° |
| revolutions per day: | 13.14501420 |
| mean anomaly at epoch: | 254.0479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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