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 59909U 26145.60530604 +.00000000 +00000-0 +14436-3 0 00008
2 59909 44.9786 2.4317 0010808 131.9637 228.2118 13.99161788 03
| Epoch (UTC): | 25 May 2026 14:31:38 |
| Eccentricity: | 0.0010808 |
| inclination: | 44.9786° |
| perigee height: | 889 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 2.4317° |
| argument of perigee: | 131.9637° |
| revolutions per day: | 13.99161788 |
| mean anomaly at epoch: | 228.2118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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