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 59484U 26145.64245896 +.00000000 +00000-0 -10229-4 0 00004
2 59484 43.0018 265.2359 0001197 266.1325 93.9390 15.27589584 00
| Epoch (UTC): | 25 May 2026 15:25:08 |
| Eccentricity: | 0.0001197 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 265.2359° |
| argument of perigee: | 266.1325° |
| revolutions per day: | 15.27589584 |
| mean anomaly at epoch: | 93.9390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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