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 06829U 26100.21981615 +.00000000 +00000-0 +41293-4 0 00003
2 06829 82.9445 170.9174 0022085 218.5994 161.6170 13.77453495 03
| Epoch (UTC): | 10 April 2026 05:16:32 |
| Eccentricity: | 0.0022085 |
| inclination: | 82.9445° |
| perigee height: | 957 km |
| apogee height: | 989 km |
| right ascension of ascending node: | 170.9174° |
| argument of perigee: | 218.5994° |
| revolutions per day: | 13.77453495 |
| mean anomaly at epoch: | 161.6170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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