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 26133.53730666 +.00000000 +00000-0 +49278-4 0 00009
2 00029 48.3769 189.3138 0021588 120.4558 239.8491 14.78732015 06
| Epoch (UTC): | 13 May 2026 12:53:43 |
| Eccentricity: | 0.0021588 |
| inclination: | 48.3769° |
| perigee height: | 618 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 189.3138° |
| argument of perigee: | 120.4558° |
| revolutions per day: | 14.78732015 |
| mean anomaly at epoch: | 239.8491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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