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 58907U 26145.48489718 +.00000000 +00000-0 +20429-3 0 00009
2 58907 50.0011 71.6889 0006302 308.2954 51.7422 14.96958767 02
| Epoch (UTC): | 25 May 2026 11:38:15 |
| Eccentricity: | 0.0006302 |
| inclination: | 50.0011° |
| perigee height: | 572 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 71.6889° |
| argument of perigee: | 308.2954° |
| revolutions per day: | 14.96958767 |
| mean anomaly at epoch: | 51.7422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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