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 58409U 26145.46697351 +.00000000 +00000-0 +30698-4 0 00008
2 58409 43.0030 193.8690 0001725 268.6666 91.3988 15.27577294 06
| Epoch (UTC): | 25 May 2026 11:12:26 |
| Eccentricity: | 0.0001725 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.8690° |
| argument of perigee: | 268.6666° |
| revolutions per day: | 15.27577294 |
| mean anomaly at epoch: | 91.3988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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