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 43803U 26072.60945062 +.00000000 +00000-0 +69571-3 0 00001
2 43803 97.4248 135.2859 0004924 239.8747 120.2006 15.30462837 06
| Epoch (UTC): | 13 March 2026 14:37:36 |
| Eccentricity: | 0.0004924 |
| inclination: | 97.4248° |
| perigee height: | 471 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 135.2859° |
| argument of perigee: | 239.8747° |
| revolutions per day: | 15.30462837 |
| mean anomaly at epoch: | 120.2006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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