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 54219U 26145.54258854 +.00000000 +00000-0 +00000-0 0 00003
2 54219 5.5609 63.8374 0001318 92.5749 103.6643 1.00523971 09
| Epoch (UTC): | 25 May 2026 13:01:19 |
| Eccentricity: | 0.0001318 |
| inclination: | 5.5609° |
| perigee height: | 35711 km |
| apogee height: | 35722 km |
| right ascension of ascending node: | 63.8374° |
| argument of perigee: | 92.5749° |
| revolutions per day: | 1.00523971 |
| mean anomaly at epoch: | 103.6643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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