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 14440U 26104.84050389 +.00000000 +00000-0 +81932-3 0 00002
2 14440 82.9189 242.6439 0113161 222.8221 292.7945 13.64422818 01
| Epoch (UTC): | 14 April 2026 20:10:19 |
| Eccentricity: | 0.0113161 |
| inclination: | 82.9189° |
| perigee height: | 936 km |
| apogee height: | 1103 km |
| right ascension of ascending node: | 242.6439° |
| argument of perigee: | 222.8221° |
| revolutions per day: | 13.64422818 |
| mean anomaly at epoch: | 292.7945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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