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 54842U 26145.45678105 +.00000000 +00000-0 +61173-5 0 00003
2 54842 43.0034 59.1240 0000924 252.4922 107.5829 15.27576320 01
| Epoch (UTC): | 25 May 2026 10:57:45 |
| Eccentricity: | 0.0000924 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 59.1240° |
| argument of perigee: | 252.4922° |
| revolutions per day: | 15.27576320 |
| mean anomaly at epoch: | 107.5829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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