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 58854U 26145.45120317 +.00000000 +00000-0 +12303-4 0 00007
2 58854 42.9998 175.2771 0001135 274.7563 85.3159 15.27576913 04
| Epoch (UTC): | 25 May 2026 10:49:43 |
| Eccentricity: | 0.0001135 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.2771° |
| argument of perigee: | 274.7563° |
| revolutions per day: | 15.27576913 |
| mean anomaly at epoch: | 85.3159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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