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 40054U 26088.20866539 +.00000000 +00000-0 +11410-2 0 00008
2 40054 98.2442 354.8756 0010634 124.8362 235.3865 15.07180829 05
| Epoch (UTC): | 29 March 2026 05:00:28 |
| Eccentricity: | 0.0010634 |
| inclination: | 98.2442° |
| perigee height: | 537 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 354.8756° |
| argument of perigee: | 124.8362° |
| revolutions per day: | 15.07180829 |
| mean anomaly at epoch: | 235.3865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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