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 54798U 26145.39674405 +.00000000 +00000-0 -85424-5 0 00001
2 54798 53.2129 34.5319 0001273 84.3434 275.7704 15.08833859 03
| Epoch (UTC): | 25 May 2026 09:31:18 |
| Eccentricity: | 0.0001273 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.5319° |
| argument of perigee: | 84.3434° |
| revolutions per day: | 15.08833859 |
| mean anomaly at epoch: | 275.7704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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