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 26032.38061363 +.00000000 +00000-0 +54517-3 0 00002
2 40034 97.7571 190.4032 0044939 145.0309 215.3874 14.89756712 09
| Epoch (UTC): | 01 February 2026 09:08:05 |
| Eccentricity: | 0.0044939 |
| inclination: | 97.7571° |
| perigee height: | 567 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 190.4032° |
| argument of perigee: | 145.0309° |
| revolutions per day: | 14.89756712 |
| mean anomaly at epoch: | 215.3874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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