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 58422U 26145.49202502 +.00000000 +00000-0 +77222-4 0 00000
2 58422 43.0008 196.5580 0001642 275.9249 84.1416 15.27578208 02
| Epoch (UTC): | 25 May 2026 11:48:30 |
| Eccentricity: | 0.0001642 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 196.5580° |
| argument of perigee: | 275.9249° |
| revolutions per day: | 15.27578208 |
| mean anomaly at epoch: | 84.1416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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