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 40034U 26109.26571455 +.00000000 +00000-0 +29287-3 0 00008
2 40034 97.7711 265.9497 0042361 250.8271 108.8360 14.90471491 04
| Epoch (UTC): | 19 April 2026 06:22:37 |
| Eccentricity: | 0.0042361 |
| inclination: | 97.7711° |
| perigee height: | 567 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 265.9497° |
| argument of perigee: | 250.8271° |
| revolutions per day: | 14.90471491 |
| mean anomaly at epoch: | 108.8360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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