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 58700U 26145.62035234 +.00000000 +00000-0 +20107-3 0 00009
2 58700 97.4675 331.8109 0008489 73.8482 286.3691 15.26748863 01
| Epoch (UTC): | 25 May 2026 14:53:18 |
| Eccentricity: | 0.0008489 |
| inclination: | 97.4675° |
| perigee height: | 480 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 331.8109° |
| argument of perigee: | 73.8482° |
| revolutions per day: | 15.26748863 |
| mean anomaly at epoch: | 286.3691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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