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 58244U 26145.45568073 +.00000000 +00000-0 +90262-4 0 00005
2 58244 43.0019 211.8002 0001800 263.1750 96.8897 15.27577006 06
| Epoch (UTC): | 25 May 2026 10:56:10 |
| Eccentricity: | 0.0001800 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.8002° |
| argument of perigee: | 263.1750° |
| revolutions per day: | 15.27577006 |
| mean anomaly at epoch: | 96.8897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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