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 58670U 26145.02795706 +.00000000 +00000-0 +95622-4 0 00001
2 58670 43.0067 13.8116 0001285 266.1560 93.9145 15.27585233 02
| Epoch (UTC): | 25 May 2026 00:40:15 |
| Eccentricity: | 0.0001285 |
| inclination: | 43.0067° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 13.8116° |
| argument of perigee: | 266.1560° |
| revolutions per day: | 15.27585233 |
| mean anomaly at epoch: | 93.9145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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