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 56058U 26145.49841147 +.00000000 +00000-0 +74365-4 0 00002
2 56058 87.9105 233.2858 0003299 95.6204 264.5303 13.16595995 02
| Epoch (UTC): | 25 May 2026 11:57:42 |
| Eccentricity: | 0.0003299 |
| inclination: | 87.9105° |
| perigee height: | 1195 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 233.2858° |
| argument of perigee: | 95.6204° |
| revolutions per day: | 13.16595995 |
| mean anomaly at epoch: | 264.5303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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