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 58111U 26145.32997378 +.00000000 +00000-0 +14628-4 0 00000
2 58111 53.1598 169.6844 0001250 83.9016 276.2127 15.30191582 04
| Epoch (UTC): | 25 May 2026 07:55:09 |
| Eccentricity: | 0.0001250 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.6844° |
| argument of perigee: | 83.9016° |
| revolutions per day: | 15.30191582 |
| mean anomaly at epoch: | 276.2127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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