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 29495U 26106.19211300 +.00000000 +00000-0 +00000-0 0 00004
2 29495 2.8746 80.3877 0003804 305.7452 39.3854 1.00271672 00
| Epoch (UTC): | 16 April 2026 04:36:38 |
| Eccentricity: | 0.0003804 |
| inclination: | 2.8746° |
| perigee height: | 35771 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 80.3877° |
| argument of perigee: | 305.7452° |
| revolutions per day: | 1.00271672 |
| mean anomaly at epoch: | 39.3854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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