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 65959U 26145.35251382 +.00000000 +00000-0 +27525-3 0 00008
2 65959 51.9040 11.6262 0000818 101.8531 258.2523 14.79932646 07
| Epoch (UTC): | 25 May 2026 08:27:37 |
| Eccentricity: | 0.0000818 |
| inclination: | 51.9040° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 11.6262° |
| argument of perigee: | 101.8531° |
| revolutions per day: | 14.79932646 |
| mean anomaly at epoch: | 258.2523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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