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 48439U 26145.38797010 +.00000000 +00000-0 +71223-6 0 00005
2 48439 53.1591 181.6612 0001314 92.1277 267.9875 15.31708535 08
| Epoch (UTC): | 25 May 2026 09:18:40 |
| Eccentricity: | 0.0001314 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 181.6612° |
| argument of perigee: | 92.1277° |
| revolutions per day: | 15.31708535 |
| mean anomaly at epoch: | 267.9875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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