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 54803U 26145.46252186 +.00000000 +00000-0 +55239-3 0 00002
2 54803 53.2129 59.1365 0001466 98.2855 261.8304 15.08799611 08
| Epoch (UTC): | 25 May 2026 11:06:01 |
| Eccentricity: | 0.0001466 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 59.1365° |
| argument of perigee: | 98.2855° |
| revolutions per day: | 15.08799611 |
| mean anomaly at epoch: | 261.8304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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