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 43719U 26145.60982476 +.00000000 +00000-0 +18122-3 0 00004
2 43719 97.9843 212.5333 0001194 119.0115 241.1216 14.78639719 00
| Epoch (UTC): | 25 May 2026 14:38:08 |
| Eccentricity: | 0.0001194 |
| inclination: | 97.9843° |
| perigee height: | 633 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 212.5333° |
| argument of perigee: | 119.0115° |
| revolutions per day: | 14.78639719 |
| mean anomaly at epoch: | 241.1216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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