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 00020U 26104.40421595 +.00000000 +00000-0 +14207-3 0 00005
2 00020 33.3387 136.5836 1637332 71.6379 305.4879 11.61922327 01
| Epoch (UTC): | 14 April 2026 09:42:04 |
| Eccentricity: | 0.1637332 |
| inclination: | 33.3387° |
| perigee height: | 508 km |
| apogee height: | 3204 km |
| right ascension of ascending node: | 136.5836° |
| argument of perigee: | 71.6379° |
| revolutions per day: | 11.61922327 |
| mean anomaly at epoch: | 305.4879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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