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 58841U 26145.56030361 +.00000000 +00000-0 -42533-5 0 00004
2 58841 53.1603 207.3914 0001113 85.6082 274.5046 15.30188391 04
| Epoch (UTC): | 25 May 2026 13:26:50 |
| Eccentricity: | 0.0001113 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.3914° |
| argument of perigee: | 85.6082° |
| revolutions per day: | 15.30188391 |
| mean anomaly at epoch: | 274.5046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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