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 48473U 26145.43296185 +.00000000 +00000-0 +27238-4 0 00001
2 48473 53.1594 194.0663 0001303 77.1427 282.9720 15.31700748 05
| Epoch (UTC): | 25 May 2026 10:23:27 |
| Eccentricity: | 0.0001303 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 194.0663° |
| argument of perigee: | 77.1427° |
| revolutions per day: | 15.31700748 |
| mean anomaly at epoch: | 282.9720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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