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 54771U 26145.47218448 +.00000000 +00000-0 +92582-4 0 00003
2 54771 53.2147 54.2276 0001363 86.0477 274.0671 15.08835733 09
| Epoch (UTC): | 25 May 2026 11:19:56 |
| Eccentricity: | 0.0001363 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 54.2276° |
| argument of perigee: | 86.0477° |
| revolutions per day: | 15.08835733 |
| mean anomaly at epoch: | 274.0671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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