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 59944U 26145.60108091 +.00000000 +00000-0 +49104-4 0 00009
2 59944 42.9989 258.3165 0001295 267.7343 92.3360 15.27578910 01
| Epoch (UTC): | 25 May 2026 14:25:33 |
| Eccentricity: | 0.0001295 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 258.3165° |
| argument of perigee: | 267.7343° |
| revolutions per day: | 15.27578910 |
| mean anomaly at epoch: | 92.3360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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