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 58860U 26145.45763847 +.00000000 +00000-0 +65845-4 0 00004
2 58860 43.0021 175.3292 0001249 274.2582 85.8127 15.27581509 08
| Epoch (UTC): | 25 May 2026 10:58:59 |
| Eccentricity: | 0.0001249 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.3292° |
| argument of perigee: | 274.2582° |
| revolutions per day: | 15.27581509 |
| mean anomaly at epoch: | 85.8127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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