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 48791U 26145.31665763 +.00000000 +00000-0 +60951-3 0 00001
2 48791 87.8999 263.7433 0001891 101.8637 258.2705 13.15548911 01
| Epoch (UTC): | 25 May 2026 07:35:59 |
| Eccentricity: | 0.0001891 |
| inclination: | 87.8999° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7433° |
| argument of perigee: | 101.8637° |
| revolutions per day: | 13.15548911 |
| mean anomaly at epoch: | 258.2705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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