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 48241U 26145.66729544 +.00000000 +00000-0 -45490-3 0 00009
2 48241 87.8941 294.2054 0002064 104.2342 255.9017 13.14503202 02
| Epoch (UTC): | 25 May 2026 16:00:54 |
| Eccentricity: | 0.0002064 |
| inclination: | 87.8941° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2054° |
| argument of perigee: | 104.2342° |
| revolutions per day: | 13.14503202 |
| mean anomaly at epoch: | 255.9017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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