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 48483U 26145.42006086 +.00000000 +00000-0 +34024-4 0 00001
2 48483 53.1597 197.2118 0001207 81.8881 278.2257 15.31702873 02
| Epoch (UTC): | 25 May 2026 10:04:53 |
| Eccentricity: | 0.0001207 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 197.2118° |
| argument of perigee: | 81.8881° |
| revolutions per day: | 15.31702873 |
| mean anomaly at epoch: | 278.2257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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