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 00029U 26100.08922216 +.00000000 +00000-0 +10148-3 0 00000
2 00029 48.3800 348.2593 0022427 334.4566 25.5238 14.78692194 04
| Epoch (UTC): | 10 April 2026 02:08:28 |
| Eccentricity: | 0.0022427 |
| inclination: | 48.3800° |
| perigee height: | 618 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 348.2593° |
| argument of perigee: | 334.4566° |
| revolutions per day: | 14.78692194 |
| mean anomaly at epoch: | 25.5238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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