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 55009U 26109.23929272 +.00000000 +00000-0 +31582-3 0 00008
2 55009 97.3213 173.5236 0004727 341.3540 18.7533 15.41016978 02
| Epoch (UTC): | 19 April 2026 05:44:34 |
| Eccentricity: | 0.0004727 |
| inclination: | 97.3213° |
| perigee height: | 440 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 173.5236° |
| argument of perigee: | 341.3540° |
| revolutions per day: | 15.41016978 |
| mean anomaly at epoch: | 18.7533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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