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 26045.55606580 +.00000000 +00000-0 +13331-3 0 00000
2 00029 48.3769 247.3697 0021888 100.9660 259.3717 14.78578432 00
| Epoch (UTC): | 14 February 2026 13:20:44 |
| Eccentricity: | 0.0021888 |
| inclination: | 48.3769° |
| perigee height: | 618 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 247.3697° |
| argument of perigee: | 100.9660° |
| revolutions per day: | 14.78578432 |
| mean anomaly at epoch: | 259.3717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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