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 57991U 26145.55977079 +.00000000 +00000-0 +52716-4 0 00006
2 57991 43.0066 352.8556 0002033 271.4128 88.6491 15.27574468 04
| Epoch (UTC): | 25 May 2026 13:26:04 |
| Eccentricity: | 0.0002033 |
| inclination: | 43.0066° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.8556° |
| argument of perigee: | 271.4128° |
| revolutions per day: | 15.27574468 |
| mean anomaly at epoch: | 88.6491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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