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 58247U 26145.57488587 +.00000000 +00000-0 +47222-4 0 00000
2 58247 43.0027 210.9750 0001820 268.7191 91.3453 15.27579559 03
| Epoch (UTC): | 25 May 2026 13:47:50 |
| Eccentricity: | 0.0001820 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 210.9750° |
| argument of perigee: | 268.7191° |
| revolutions per day: | 15.27579559 |
| mean anomaly at epoch: | 91.3453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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