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 18586U 26039.95242242 +.00000000 +00000-0 +62667-4 0 00002
2 18586 74.0036 234.7287 0021533 264.8318 95.0379 14.38303576 02
| Epoch (UTC): | 08 February 2026 22:51:29 |
| Eccentricity: | 0.0021533 |
| inclination: | 74.0036° |
| perigee height: | 749 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 234.7287° |
| argument of perigee: | 264.8318° |
| revolutions per day: | 14.38303576 |
| mean anomaly at epoch: | 95.0379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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