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 26103.12506375 +.00000000 +00000-0 +17747-3 0 00009
2 18214 82.5124 166.8398 0015859 297.2312 62.7316 15.36240336 03
| Epoch (UTC): | 13 April 2026 03:00:05 |
| Eccentricity: | 0.0015859 |
| inclination: | 82.5124° |
| perigee height: | 446 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 166.8398° |
| argument of perigee: | 297.2312° |
| revolutions per day: | 15.36240336 |
| mean anomaly at epoch: | 62.7316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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