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 59488U 26144.76978181 +.00000000 +00000-0 +80472-5 0 00007
2 59488 43.0017 277.6533 0001154 279.9505 80.1216 15.27574232 08
| Epoch (UTC): | 24 May 2026 18:28:29 |
| Eccentricity: | 0.0001154 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.6533° |
| argument of perigee: | 279.9505° |
| revolutions per day: | 15.27574232 |
| mean anomaly at epoch: | 80.1216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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