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 26048.93494823 +.00000000 +00000-0 +11626-3 0 00005
2 00029 48.3766 231.3163 0021936 115.9016 244.4162 14.78584018 09
| Epoch (UTC): | 17 February 2026 22:26:19 |
| Eccentricity: | 0.0021936 |
| inclination: | 48.3766° |
| perigee height: | 618 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 231.3163° |
| argument of perigee: | 115.9016° |
| revolutions per day: | 14.78584018 |
| mean anomaly at epoch: | 244.4162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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