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 48557U 26145.32375707 +.00000000 +00000-0 +92765-5 0 00008
2 48557 53.1588 130.4286 0001269 96.3918 263.7228 15.31703421 06
| Epoch (UTC): | 25 May 2026 07:46:12 |
| Eccentricity: | 0.0001269 |
| inclination: | 53.1588° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 130.4286° |
| argument of perigee: | 96.3918° |
| revolutions per day: | 15.31703421 |
| mean anomaly at epoch: | 263.7228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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