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 14781U 26105.86347981 +.00000000 +00000-0 +84603-4 0 00009
2 14781 97.8006 72.1616 0008540 39.2959 320.8877 14.90632276 05
| Epoch (UTC): | 15 April 2026 20:43:24 |
| Eccentricity: | 0.0008540 |
| inclination: | 97.8006° |
| perigee height: | 590 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 72.1616° |
| argument of perigee: | 39.2959° |
| revolutions per day: | 14.90632276 |
| mean anomaly at epoch: | 320.8877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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