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 29051U 26053.71145850 +.00000000 +00000-0 +18576-3 0 00007
2 29051 72.0043 175.8431 0067814 288.8771 70.5022 14.31435360 07
| Epoch (UTC): | 22 February 2026 17:04:30 |
| Eccentricity: | 0.0067814 |
| inclination: | 72.0043° |
| perigee height: | 738 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 175.8431° |
| argument of perigee: | 288.8771° |
| revolutions per day: | 14.31435360 |
| mean anomaly at epoch: | 70.5022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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