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 48235U 26145.64494436 +.00000000 +00000-0 +42724-3 0 00005
2 48235 87.8957 294.1943 0001704 94.5245 265.6080 13.14500938 02
| Epoch (UTC): | 25 May 2026 15:28:43 |
| Eccentricity: | 0.0001704 |
| inclination: | 87.8957° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.1943° |
| argument of perigee: | 94.5245° |
| revolutions per day: | 13.14500938 |
| mean anomaly at epoch: | 265.6080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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