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 57055U 26144.98892745 +.00000000 +00000-0 -11319-4 0 00004
2 57055 43.0047 39.5699 0001286 266.0517 94.0187 15.27568318 02
| Epoch (UTC): | 24 May 2026 23:44:03 |
| Eccentricity: | 0.0001286 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 39.5699° |
| argument of perigee: | 266.0517° |
| revolutions per day: | 15.27568318 |
| mean anomaly at epoch: | 94.0187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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