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 39417U 26110.34162080 +.00000000 +00000-0 +24891-3 0 00008
2 39417 97.8133 72.3703 0044702 85.7181 274.9149 15.00695104 03
| Epoch (UTC): | 20 April 2026 08:11:56 |
| Eccentricity: | 0.0044702 |
| inclination: | 97.8133° |
| perigee height: | 534 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 72.3703° |
| argument of perigee: | 85.7181° |
| revolutions per day: | 15.00695104 |
| mean anomaly at epoch: | 274.9149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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