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 58034U 26145.24869124 +.00000000 +00000-0 -62976-4 0 00002
2 58034 53.1596 82.8669 0001115 80.8653 279.2474 15.30212208 07
| Epoch (UTC): | 25 May 2026 05:58:06 |
| Eccentricity: | 0.0001115 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 82.8669° |
| argument of perigee: | 80.8653° |
| revolutions per day: | 15.30212208 |
| mean anomaly at epoch: | 279.2474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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