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 58346U 26140.72351743 +.00000000 +00000-0 +00000-0 0 00004
2 58346 0.0469 12.7092 0004726 60.9652 286.3772 5.00115437 06
| Epoch (UTC): | 20 May 2026 17:21:51 |
| Eccentricity: | 0.0004726 |
| inclination: | 0.0469° |
| perigee height: | 8059 km |
| apogee height: | 8073 km |
| right ascension of ascending node: | 12.7092° |
| argument of perigee: | 60.9652° |
| revolutions per day: | 5.00115437 |
| mean anomaly at epoch: | 286.3772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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