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 58012U 26145.61873156 +.00000000 +00000-0 +81283-5 0 00001
2 58012 43.0043 352.4150 0000804 271.7583 88.3177 15.27575905 07
| Epoch (UTC): | 25 May 2026 14:50:58 |
| Eccentricity: | 0.0000804 |
| inclination: | 43.0043° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.4150° |
| argument of perigee: | 271.7583° |
| revolutions per day: | 15.27575905 |
| mean anomaly at epoch: | 88.3177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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