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 58287U 26144.84874255 +.00000000 +00000-0 +98986-3 0 00006
2 58287 97.3778 240.1117 0004627 196.4700 163.6416 15.75235146 01
| Epoch (UTC): | 24 May 2026 20:22:11 |
| Eccentricity: | 0.0004627 |
| inclination: | 97.3778° |
| perigee height: | 341 km |
| apogee height: | 347 km |
| right ascension of ascending node: | 240.1117° |
| argument of perigee: | 196.4700° |
| revolutions per day: | 15.75235146 |
| mean anomaly at epoch: | 163.6416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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