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 29049U 26104.20050205 +.00000000 +00000-0 +11674-3 0 00006
2 29049 72.0187 174.7807 0035156 316.1650 43.6698 14.31357525 09
| Epoch (UTC): | 14 April 2026 04:48:43 |
| Eccentricity: | 0.0035156 |
| inclination: | 72.0187° |
| perigee height: | 762 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 174.7807° |
| argument of perigee: | 316.1650° |
| revolutions per day: | 14.31357525 |
| mean anomaly at epoch: | 43.6698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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