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 48236U 26145.39109771 +.00000000 +00000-0 +52454-3 0 00004
2 48236 87.8939 294.2333 0002071 102.4702 257.6660 13.14502754 05
| Epoch (UTC): | 25 May 2026 09:23:10 |
| Eccentricity: | 0.0002071 |
| inclination: | 87.8939° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2333° |
| argument of perigee: | 102.4702° |
| revolutions per day: | 13.14502754 |
| mean anomaly at epoch: | 257.6660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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