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 58104U 26145.47745744 +.00000000 +00000-0 +12131-4 0 00003
2 58104 53.1599 168.9879 0001074 80.0318 280.0804 15.30193447 01
| Epoch (UTC): | 25 May 2026 11:27:32 |
| Eccentricity: | 0.0001074 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.9879° |
| argument of perigee: | 80.0318° |
| revolutions per day: | 15.30193447 |
| mean anomaly at epoch: | 280.0804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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