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 26066.61262844 +.00000000 +00000-0 +86910-4 0 00004
2 54029 98.2778 73.1407 0015251 48.3776 311.8723 14.52011094 06
| Epoch (UTC): | 07 March 2026 14:42:11 |
| Eccentricity: | 0.0015251 |
| inclination: | 98.2778° |
| perigee height: | 708 km |
| apogee height: | 730 km |
| right ascension of ascending node: | 73.1407° |
| argument of perigee: | 48.3776° |
| revolutions per day: | 14.52011094 |
| mean anomaly at epoch: | 311.8723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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