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 57953U 26144.94354087 +.00000000 +00000-0 +48936-4 0 00003
2 57953 53.1603 20.0155 0001076 73.2747 286.8371 15.30189745 04
| Epoch (UTC): | 24 May 2026 22:38:41 |
| Eccentricity: | 0.0001076 |
| inclination: | 53.1603° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 20.0155° |
| argument of perigee: | 73.2747° |
| revolutions per day: | 15.30189745 |
| mean anomaly at epoch: | 286.8371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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