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 48792U 26145.31585481 +.00000000 +00000-0 +42192-3 0 00007
2 48792 87.8996 263.7446 0001789 100.1468 259.9864 13.15547185 09
| Epoch (UTC): | 25 May 2026 07:34:49 |
| Eccentricity: | 0.0001789 |
| inclination: | 87.8996° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7446° |
| argument of perigee: | 100.1468° |
| revolutions per day: | 13.15547185 |
| mean anomaly at epoch: | 259.9864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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