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 18214U 26017.14827014 +.00000000 +00000-0 +28653-3 0 00009
2 18214 82.5109 254.1569 0016813 243.9639 115.9873 15.33933735 06
| Epoch (UTC): | 17 January 2026 03:33:30 |
| Eccentricity: | 0.0016813 |
| inclination: | 82.5109° |
| perigee height: | 453 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 254.1569° |
| argument of perigee: | 243.9639° |
| revolutions per day: | 15.33933735 |
| mean anomaly at epoch: | 115.9873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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