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 26049.54314512 +.00000000 +00000-0 +12008-3 0 00004
2 00029 48.3765 228.4264 0021930 118.6027 241.7096 14.78585309 03
| Epoch (UTC): | 18 February 2026 13:02:07 |
| Eccentricity: | 0.0021930 |
| inclination: | 48.3765° |
| perigee height: | 618 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 228.4264° |
| argument of perigee: | 118.6027° |
| revolutions per day: | 14.78585309 |
| mean anomaly at epoch: | 241.7096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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