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 43678U 26071.32390602 +.00000000 +00000-0 +14519-3 0 00005
2 43678 98.1043 263.4680 0012102 119.1115 241.1320 14.99974799 00
| Epoch (UTC): | 12 March 2026 07:46:25 |
| Eccentricity: | 0.0012102 |
| inclination: | 98.1043° |
| perigee height: | 559 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 263.4680° |
| argument of perigee: | 119.1115° |
| revolutions per day: | 14.99974799 |
| mean anomaly at epoch: | 241.1320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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