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 51657U 26067.07613632 +.00000000 +00000-0 +10573-2 0 00004
2 51657 97.4478 114.4161 0004389 95.4269 264.7498 15.77926845 06
| Epoch (UTC): | 08 March 2026 01:49:38 |
| Eccentricity: | 0.0004389 |
| inclination: | 97.4478° |
| perigee height: | 333 km |
| apogee height: | 339 km |
| right ascension of ascending node: | 114.4161° |
| argument of perigee: | 95.4269° |
| revolutions per day: | 15.77926845 |
| mean anomaly at epoch: | 264.7498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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