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 29271U 26065.17036212 +.00000000 +00000-0 +83611-3 0 00007
2 29271 49.5528 21.4138 5183067 199.2333 130.2934 5.32936388 04
| Epoch (UTC): | 06 March 2026 04:05:19 |
| Eccentricity: | 0.5183067 |
| inclination: | 49.5528° |
| perigee height: | 291 km |
| apogee height: | 14642 km |
| right ascension of ascending node: | 21.4138° |
| argument of perigee: | 199.2333° |
| revolutions per day: | 5.32936388 |
| mean anomaly at epoch: | 130.2934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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