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 26053.67116123 +.00000000 +00000-0 +13953-3 0 00004
2 29049 72.0170 278.1256 0032477 44.5347 315.8392 14.31305626 06
| Epoch (UTC): | 22 February 2026 16:06:28 |
| Eccentricity: | 0.0032477 |
| inclination: | 72.0170° |
| perigee height: | 764 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 278.1256° |
| argument of perigee: | 44.5347° |
| revolutions per day: | 14.31305626 |
| mean anomaly at epoch: | 315.8392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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