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 54802U 26145.64086427 +.00000000 +00000-0 +50059-4 0 00000
2 54802 53.2189 3.1529 0001299 62.4094 297.7029 15.08005411 06
| Epoch (UTC): | 25 May 2026 15:22:50 |
| Eccentricity: | 0.0001299 |
| inclination: | 53.2189° |
| perigee height: | 541 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 3.1529° |
| argument of perigee: | 62.4094° |
| revolutions per day: | 15.08005411 |
| mean anomaly at epoch: | 297.7029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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