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 48055U 26145.22424622 +.00000000 +00000-0 -62695-3 0 00009
2 48055 87.8951 324.7962 0001602 103.6702 256.4606 13.13468958 00
| Epoch (UTC): | 25 May 2026 05:22:54 |
| Eccentricity: | 0.0001602 |
| inclination: | 87.8951° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7962° |
| argument of perigee: | 103.6702° |
| revolutions per day: | 13.13468958 |
| mean anomaly at epoch: | 256.4606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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