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 18665U 26038.14077190 +.00000000 +00000-0 +63895-4 0 00002
2 18665 66.0841 29.8597 0036408 193.0112 167.0058 14.55610517 03
| Epoch (UTC): | 07 February 2026 03:22:42 |
| Eccentricity: | 0.0036408 |
| inclination: | 66.0841° |
| perigee height: | 682 km |
| apogee height: | 733 km |
| right ascension of ascending node: | 29.8597° |
| argument of perigee: | 193.0112° |
| revolutions per day: | 14.55610517 |
| mean anomaly at epoch: | 167.0058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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