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 47773U 26145.35519485 +.00000000 +00000-0 +23787-4 0 00000
2 47773 53.1577 220.1579 0001053 91.9011 268.2111 15.31707913 02
| Epoch (UTC): | 25 May 2026 08:31:28 |
| Eccentricity: | 0.0001053 |
| inclination: | 53.1577° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 220.1579° |
| argument of perigee: | 91.9011° |
| revolutions per day: | 15.31707913 |
| mean anomaly at epoch: | 268.2111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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