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 20439U 26100.07011477 +.00000000 +00000-0 +63148-4 0 00003
2 20439 98.8595 134.1299 0011645 73.8114 348.0247 14.33915188 05
| Epoch (UTC): | 10 April 2026 01:40:57 |
| Eccentricity: | 0.0011645 |
| inclination: | 98.8595° |
| perigee height: | 770 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 134.1299° |
| argument of perigee: | 73.8114° |
| revolutions per day: | 14.33915188 |
| mean anomaly at epoch: | 348.0247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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