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 58673U 26145.03325669 +.00000000 +00000-0 +32489-4 0 00004
2 58673 43.0008 3.3345 0000825 272.0316 88.0441 15.27582286 01
| Epoch (UTC): | 25 May 2026 00:47:53 |
| Eccentricity: | 0.0000825 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.3345° |
| argument of perigee: | 272.0316° |
| revolutions per day: | 15.27582286 |
| mean anomaly at epoch: | 88.0441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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