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 58417U 26145.53717220 +.00000000 +00000-0 +50222-4 0 00008
2 58417 43.0037 338.1324 0001402 262.8599 97.2093 15.27577490 03
| Epoch (UTC): | 25 May 2026 12:53:31 |
| Eccentricity: | 0.0001402 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.1324° |
| argument of perigee: | 262.8599° |
| revolutions per day: | 15.27577490 |
| mean anomaly at epoch: | 97.2093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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