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 59920U 26145.61396096 +.00000000 +00000-0 +23450-3 0 00003
2 59920 97.5832 164.3488 0009973 302.9850 57.0427 15.22325043 02
| Epoch (UTC): | 25 May 2026 14:44:06 |
| Eccentricity: | 0.0009973 |
| inclination: | 97.5832° |
| perigee height: | 492 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 164.3488° |
| argument of perigee: | 302.9850° |
| revolutions per day: | 15.22325043 |
| mean anomaly at epoch: | 57.0427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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