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 48482U 26145.40605432 +.00000000 +00000-0 +26352-4 0 00003
2 48482 53.1596 197.0958 0001214 89.2005 270.9136 15.31697126 07
| Epoch (UTC): | 25 May 2026 09:44:43 |
| Eccentricity: | 0.0001214 |
| inclination: | 53.1596° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 197.0958° |
| argument of perigee: | 89.2005° |
| revolutions per day: | 15.31697126 |
| mean anomaly at epoch: | 270.9136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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