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 47621U 26145.19328161 +.00000000 +00000-0 +14687-2 0 00000
2 47621 53.1583 65.4092 0004974 92.3952 267.7624 15.43300474 02
| Epoch (UTC): | 25 May 2026 04:38:19 |
| Eccentricity: | 0.0004974 |
| inclination: | 53.1583° |
| perigee height: | 433 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 65.4092° |
| argument of perigee: | 92.3952° |
| revolutions per day: | 15.43300474 |
| mean anomaly at epoch: | 267.7624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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