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 64959U 26145.49226049 +.00000000 +00000-0 +12001-3 0 00007
2 64959 86.4943 290.1416 0001892 97.9354 262.1995 13.24406288 01
| Epoch (UTC): | 25 May 2026 11:48:51 |
| Eccentricity: | 0.0001892 |
| inclination: | 86.4943° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 290.1416° |
| argument of perigee: | 97.9354° |
| revolutions per day: | 13.24406288 |
| mean anomaly at epoch: | 262.1995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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