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 59348U 26145.43716970 +.00000000 +00000-0 +14613-4 0 00006
2 59348 43.0011 175.7635 0001240 273.3560 86.7150 15.27577379 07
| Epoch (UTC): | 25 May 2026 10:29:31 |
| Eccentricity: | 0.0001240 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.7635° |
| argument of perigee: | 273.3560° |
| revolutions per day: | 15.27577379 |
| mean anomaly at epoch: | 86.7150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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