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 26069.10730412 +.00000000 +00000-0 +85955-3 0 00000
2 29271 49.5533 18.2542 5182888 201.9222 123.9384 5.32984247 06
| Epoch (UTC): | 10 March 2026 02:34:31 |
| Eccentricity: | 0.5182888 |
| inclination: | 49.5533° |
| perigee height: | 291 km |
| apogee height: | 14641 km |
| right ascension of ascending node: | 18.2542° |
| argument of perigee: | 201.9222° |
| revolutions per day: | 5.32984247 |
| mean anomaly at epoch: | 123.9384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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