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 58226U 26145.27214817 +.00000000 +00000-0 -96072-5 0 00006
2 58226 43.0030 110.5110 0000400 168.9489 191.1372 15.27552453 06
| Epoch (UTC): | 25 May 2026 06:31:53 |
| Eccentricity: | 0.0000400 |
| inclination: | 43.0030° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 110.5110° |
| argument of perigee: | 168.9489° |
| revolutions per day: | 15.27552453 |
| mean anomaly at epoch: | 191.1372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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