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 58286U 26145.14468434 +.00000000 +00000-0 +52197-3 0 00001
2 58286 97.3930 236.7024 0005130 209.9650 150.1311 15.55991675 01
| Epoch (UTC): | 25 May 2026 03:28:20 |
| Eccentricity: | 0.0005130 |
| inclination: | 97.3930° |
| perigee height: | 396 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 236.7024° |
| argument of perigee: | 209.9650° |
| revolutions per day: | 15.55991675 |
| mean anomaly at epoch: | 150.1311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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