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 58705U 26145.57834488 +.00000000 +00000-0 +12991-4 0 00009
2 58705 53.1602 254.9816 0001013 89.8682 270.2452 15.69704018 08
| Epoch (UTC): | 25 May 2026 13:52:48 |
| Eccentricity: | 0.0001013 |
| inclination: | 53.1602° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 254.9816° |
| argument of perigee: | 89.8682° |
| revolutions per day: | 15.69704018 |
| mean anomaly at epoch: | 270.2452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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