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 48428U 26145.48590189 +.00000000 +00000-0 -29811-4 0 00007
2 48428 53.1585 181.5475 0001325 84.2688 275.8465 15.31707009 03
| Epoch (UTC): | 25 May 2026 11:39:41 |
| Eccentricity: | 0.0001325 |
| inclination: | 53.1585° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 181.5475° |
| argument of perigee: | 84.2688° |
| revolutions per day: | 15.31707009 |
| mean anomaly at epoch: | 275.8465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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