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 58109U 26145.44793947 +.00000000 +00000-0 +18827-4 0 00001
2 58109 53.1590 168.9949 0001121 95.6484 264.4644 15.30192358 02
| Epoch (UTC): | 25 May 2026 10:45:01 |
| Eccentricity: | 0.0001121 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.9949° |
| argument of perigee: | 95.6484° |
| revolutions per day: | 15.30192358 |
| mean anomaly at epoch: | 264.4644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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