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 54029U 26114.84948257 +.00000000 +00000-0 +47631-4 0 00009
2 54029 98.2772 120.6923 0013023 255.3318 104.6434 14.52035567 06
| Epoch (UTC): | 24 April 2026 20:23:15 |
| Eccentricity: | 0.0013023 |
| inclination: | 98.2772° |
| perigee height: | 710 km |
| apogee height: | 728 km |
| right ascension of ascending node: | 120.6923° |
| argument of perigee: | 255.3318° |
| revolutions per day: | 14.52035567 |
| mean anomaly at epoch: | 104.6434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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