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 56047U 26145.54116816 +.00000000 +00000-0 -29062-5 0 00000
2 56047 87.9107 233.2699 0001846 107.3990 252.7343 13.16593323 00
| Epoch (UTC): | 25 May 2026 12:59:16 |
| Eccentricity: | 0.0001846 |
| inclination: | 87.9107° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2699° |
| argument of perigee: | 107.3990° |
| revolutions per day: | 13.16593323 |
| mean anomaly at epoch: | 252.7343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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