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 29228U 26153.69065042 +.00000000 +00000-0 +14341-3 0 00001
2 29228 69.9333 17.0777 0005871 305.2645 54.7971 15.13147948 09
| Epoch (UTC): | 02 June 2026 16:34:32 |
| Eccentricity: | 0.0005871 |
| inclination: | 69.9333° |
| perigee height: | 523 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 17.0777° |
| argument of perigee: | 305.2645° |
| revolutions per day: | 15.13147948 |
| mean anomaly at epoch: | 54.7971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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