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 26073.13250249 +.00000000 +00000-0 +69458-3 0 00000
2 43803 97.4250 135.8091 0004969 237.5316 122.5445 15.30483142 03
| Epoch (UTC): | 14 March 2026 03:10:48 |
| Eccentricity: | 0.0004969 |
| inclination: | 97.4250° |
| perigee height: | 471 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 135.8091° |
| argument of perigee: | 237.5316° |
| revolutions per day: | 15.30483142 |
| mean anomaly at epoch: | 122.5445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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