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 48354U 26145.02674860 +.00000000 +00000-0 +18965-3 0 00000
2 48354 53.1607 3.1711 0001125 89.3558 270.7572 15.31708557 00
| Epoch (UTC): | 25 May 2026 00:38:31 |
| Eccentricity: | 0.0001125 |
| inclination: | 53.1607° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 3.1711° |
| argument of perigee: | 89.3558° |
| revolutions per day: | 15.31708557 |
| mean anomaly at epoch: | 270.7572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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