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 59280U 26145.56992596 +.00000000 +00000-0 +64211-4 0 00004
2 59280 50.0065 178.5503 0011369 66.1148 294.0957 14.27950973 00
| Epoch (UTC): | 25 May 2026 13:40:41 |
| Eccentricity: | 0.0011369 |
| inclination: | 50.0065° |
| perigee height: | 790 km |
| apogee height: | 807 km |
| right ascension of ascending node: | 178.5503° |
| argument of perigee: | 66.1148° |
| revolutions per day: | 14.27950973 |
| mean anomaly at epoch: | 294.0957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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