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 58445U 26145.23855809 +.00000000 +00000-0 +83913-4 0 00005
2 58445 43.0040 329.1236 0001575 267.9399 92.1272 15.27582247 04
| Epoch (UTC): | 25 May 2026 05:43:31 |
| Eccentricity: | 0.0001575 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 329.1236° |
| argument of perigee: | 267.9399° |
| revolutions per day: | 15.27582247 |
| mean anomaly at epoch: | 92.1272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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