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 58236U 26145.46981852 +.00000000 +00000-0 +79712-4 0 00008
2 58236 42.9997 211.9106 0001581 266.6116 93.4555 15.27575775 01
| Epoch (UTC): | 25 May 2026 11:16:32 |
| Eccentricity: | 0.0001581 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.9106° |
| argument of perigee: | 266.6116° |
| revolutions per day: | 15.27575775 |
| mean anomaly at epoch: | 93.4555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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