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 54804U 26145.11243398 +.00000000 +00000-0 +94987-5 0 00005
2 54804 53.2140 45.5633 0001305 87.6742 272.4400 15.08833557 01
| Epoch (UTC): | 25 May 2026 02:41:54 |
| Eccentricity: | 0.0001305 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 45.5633° |
| argument of perigee: | 87.6742° |
| revolutions per day: | 15.08833557 |
| mean anomaly at epoch: | 272.4400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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