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 59910U 26145.65822215 +.00000000 +00000-0 +15138-3 0 00007
2 59910 44.9749 1.7967 0009667 135.9135 224.2470 13.99174908 00
| Epoch (UTC): | 25 May 2026 15:47:50 |
| Eccentricity: | 0.0009667 |
| inclination: | 44.9749° |
| perigee height: | 890 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 1.7967° |
| argument of perigee: | 135.9135° |
| revolutions per day: | 13.99174908 |
| mean anomaly at epoch: | 224.2470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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