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 57288U 26145.62387933 +.00000000 +00000-0 +81528-4 0 00000
2 57288 86.5046 12.5860 0015932 252.5473 107.3929 13.39540669 08
| Epoch (UTC): | 25 May 2026 14:58:23 |
| Eccentricity: | 0.0015932 |
| inclination: | 86.5046° |
| perigee height: | 1099 km |
| apogee height: | 1123 km |
| right ascension of ascending node: | 12.5860° |
| argument of perigee: | 252.5473° |
| revolutions per day: | 13.39540669 |
| mean anomaly at epoch: | 107.3929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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