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 59837U 26145.43395161 +.00000000 +00000-0 +40092-3 0 00003
2 59837 43.0004 200.9668 0001903 273.6883 86.3751 15.27613284 05
| Epoch (UTC): | 25 May 2026 10:24:53 |
| Eccentricity: | 0.0001903 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.9668° |
| argument of perigee: | 273.6883° |
| revolutions per day: | 15.27613284 |
| mean anomaly at epoch: | 86.3751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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