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 29048U 26104.07980024 +.00000000 +00000-0 +10210-3 0 00006
2 29048 71.9679 351.2692 0043355 309.6730 50.0587 14.31340566 08
| Epoch (UTC): | 14 April 2026 01:54:54 |
| Eccentricity: | 0.0043355 |
| inclination: | 71.9679° |
| perigee height: | 756 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 351.2692° |
| argument of perigee: | 309.6730° |
| revolutions per day: | 14.31340566 |
| mean anomaly at epoch: | 50.0587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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