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 54746U 26145.66411553 +.00000000 +00000-0 +31783-3 0 00003
2 54746 34.9918 2.6351 0006481 85.0442 275.1011 15.20677338 00
| Epoch (UTC): | 25 May 2026 15:56:19 |
| Eccentricity: | 0.0006481 |
| inclination: | 34.9918° |
| perigee height: | 499 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 2.6351° |
| argument of perigee: | 85.0442° |
| revolutions per day: | 15.20677338 |
| mean anomaly at epoch: | 275.1011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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