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 26140.76735516 +.00000000 +00000-0 +42005-4 0 00002
2 00029 48.3765 154.9546 0021776 152.1451 208.0633 14.78736784 09
| Epoch (UTC): | 20 May 2026 18:24:59 |
| Eccentricity: | 0.0021776 |
| inclination: | 48.3765° |
| perigee height: | 618 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 154.9546° |
| argument of perigee: | 152.1451° |
| revolutions per day: | 14.78736784 |
| mean anomaly at epoch: | 208.0633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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