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 10829U 26070.36811795 +.00000000 +00000-0 +52094-3 0 00001
2 10829 101.7674 31.8246 0040140 293.5885 220.7654 12.36706367 08
| Epoch (UTC): | 11 March 2026 08:50:05 |
| Eccentricity: | 0.0040140 |
| inclination: | 101.7674° |
| perigee height: | 1489 km |
| apogee height: | 1552 km |
| right ascension of ascending node: | 31.8246° |
| argument of perigee: | 293.5885° |
| revolutions per day: | 12.36706367 |
| mean anomaly at epoch: | 220.7654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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