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 58864U 26145.52687008 +.00000000 +00000-0 +96864-6 0 00007
2 58864 43.0020 174.9909 0001110 275.3420 84.7305 15.27578522 08
| Epoch (UTC): | 25 May 2026 12:38:41 |
| Eccentricity: | 0.0001110 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.9909° |
| argument of perigee: | 275.3420° |
| revolutions per day: | 15.27578522 |
| mean anomaly at epoch: | 84.7305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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