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 48782U 26145.38239226 +.00000000 +00000-0 +41111-3 0 00006
2 48782 87.8992 263.7401 0001648 97.9271 262.2047 13.15547314 08
| Epoch (UTC): | 25 May 2026 09:10:38 |
| Eccentricity: | 0.0001648 |
| inclination: | 87.8992° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7401° |
| argument of perigee: | 97.9271° |
| revolutions per day: | 13.15547314 |
| mean anomaly at epoch: | 262.2047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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