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 58249U 26145.24924117 +.00000000 +00000-0 +64421-4 0 00000
2 58249 43.0022 212.8283 0001628 271.0423 89.0242 15.27575514 00
| Epoch (UTC): | 25 May 2026 05:58:54 |
| Eccentricity: | 0.0001628 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 212.8283° |
| argument of perigee: | 271.0423° |
| revolutions per day: | 15.27575514 |
| mean anomaly at epoch: | 89.0242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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