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 25359U 26064.86492368 +.00000000 +00000-0 -53718-4 0 00000
2 25359 26.3895 14.5059 0513333 230.6005 154.7697 12.94614221 08
| Epoch (UTC): | 05 March 2026 20:45:29 |
| Eccentricity: | 0.0513333 |
| inclination: | 26.3895° |
| perigee height: | 890 km |
| apogee height: | 1677 km |
| right ascension of ascending node: | 14.5059° |
| argument of perigee: | 230.6005° |
| revolutions per day: | 12.94614221 |
| mean anomaly at epoch: | 154.7697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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