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 58353U 26145.44978250 +.00000000 +00000-0 +34274-4 0 00008
2 58353 43.0014 135.3025 0001138 269.9007 90.1714 15.27579632 02
| Epoch (UTC): | 25 May 2026 10:47:41 |
| Eccentricity: | 0.0001138 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.3025° |
| argument of perigee: | 269.9007° |
| revolutions per day: | 15.27579632 |
| mean anomaly at epoch: | 90.1714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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