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 54868U 26145.12343016 +.00000000 +00000-0 +14870-4 0 00006
2 54868 43.0074 49.6161 0001769 258.9202 101.1451 15.27576990 03
| Epoch (UTC): | 25 May 2026 02:57:44 |
| Eccentricity: | 0.0001769 |
| inclination: | 43.0074° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 49.6161° |
| argument of perigee: | 258.9202° |
| revolutions per day: | 15.27576990 |
| mean anomaly at epoch: | 101.1451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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