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 59248U 26145.51440860 +.00000000 +00000-0 +48118-4 0 00003
2 59248 43.0048 69.8205 0001296 272.9912 87.0792 15.27580102 03
| Epoch (UTC): | 25 May 2026 12:20:44 |
| Eccentricity: | 0.0001296 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.8205° |
| argument of perigee: | 272.9912° |
| revolutions per day: | 15.27580102 |
| mean anomaly at epoch: | 87.0792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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