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 12586U 26138.13223457 +.00000000 +00000-0 +14337-3 0 00003
2 12586 97.6213 182.6516 0013349 113.6826 246.5818 15.34312254 02
| Epoch (UTC): | 18 May 2026 03:10:25 |
| Eccentricity: | 0.0013349 |
| inclination: | 97.6213° |
| perigee height: | 454 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 182.6516° |
| argument of perigee: | 113.6826° |
| revolutions per day: | 15.34312254 |
| mean anomaly at epoch: | 246.5818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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