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 26017.93107456 +.00000000 +00000-0 +31310-3 0 00001
2 18214 82.5106 253.3633 0016847 240.8302 119.1256 15.33949491 03
| Epoch (UTC): | 17 January 2026 22:20:44 |
| Eccentricity: | 0.0016847 |
| inclination: | 82.5106° |
| perigee height: | 453 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 253.3633° |
| argument of perigee: | 240.8302° |
| revolutions per day: | 15.33949491 |
| mean anomaly at epoch: | 119.1256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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