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 58452U 26145.50781442 +.00000000 +00000-0 +61009-4 0 00006
2 58452 43.0010 327.7067 0002260 263.4076 96.6518 15.27578068 08
| Epoch (UTC): | 25 May 2026 12:11:15 |
| Eccentricity: | 0.0002260 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 327.7067° |
| argument of perigee: | 263.4076° |
| revolutions per day: | 15.27578068 |
| mean anomaly at epoch: | 96.6518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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