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 48044U 26145.39014661 +.00000000 +00000-0 +18255-3 0 00005
2 48044 87.8940 324.7650 0001768 94.2260 265.9071 13.13469520 04
| Epoch (UTC): | 25 May 2026 09:21:48 |
| Eccentricity: | 0.0001768 |
| inclination: | 87.8940° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7650° |
| argument of perigee: | 94.2260° |
| revolutions per day: | 13.13469520 |
| mean anomaly at epoch: | 265.9071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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