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 58018U 26145.58798666 +.00000000 +00000-0 +36945-3 0 00008
2 58018 97.5539 233.7687 0002331 145.6898 214.4501 15.44341526 00
| Epoch (UTC): | 25 May 2026 14:06:42 |
| Eccentricity: | 0.0002331 |
| inclination: | 97.5539° |
| perigee height: | 432 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 233.7687° |
| argument of perigee: | 145.6898° |
| revolutions per day: | 15.44341526 |
| mean anomaly at epoch: | 214.4501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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