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 58413U 26145.56034367 +.00000000 +00000-0 +40505-4 0 00004
2 58413 43.0044 327.1684 0001353 258.8702 101.1998 15.27572704 02
| Epoch (UTC): | 25 May 2026 13:26:53 |
| Eccentricity: | 0.0001353 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.1684° |
| argument of perigee: | 258.8702° |
| revolutions per day: | 15.27572704 |
| mean anomaly at epoch: | 101.1998° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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