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 56727U 26145.47320567 +.00000000 +00000-0 +10850-3 0 00009
2 56727 86.1960 339.5828 0002572 85.6343 274.5172 14.80241204 06
| Epoch (UTC): | 25 May 2026 11:21:24 |
| Eccentricity: | 0.0002572 |
| inclination: | 86.1960° |
| perigee height: | 627 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 339.5828° |
| argument of perigee: | 85.6343° |
| revolutions per day: | 14.80241204 |
| mean anomaly at epoch: | 274.5172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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