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 58598U 26145.66668980 +.00000000 +00000-0 +29672-2 0 00003
2 58598 42.9779 51.2490 0032426 204.7509 63.2380 15.60574322 07
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0032426 |
| inclination: | 42.9779° |
| perigee height: | 364 km |
| apogee height: | 408 km |
| right ascension of ascending node: | 51.2490° |
| argument of perigee: | 204.7509° |
| revolutions per day: | 15.60574322 |
| mean anomaly at epoch: | 63.2380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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