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 26145.58293726 +.00000000 +00000-0 +61613-4 0 00004
2 54029 98.2751 150.9874 0014793 157.3984 202.7866 14.52048614 05
| Epoch (UTC): | 25 May 2026 13:59:25 |
| Eccentricity: | 0.0014793 |
| inclination: | 98.2751° |
| perigee height: | 708 km |
| apogee height: | 729 km |
| right ascension of ascending node: | 150.9874° |
| argument of perigee: | 157.3984° |
| revolutions per day: | 14.52048614 |
| mean anomaly at epoch: | 202.7866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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