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 09486U 26088.22030610 +.00000000 +00000-0 +30199-4 0 00004
2 09486 64.7003 61.7999 0074622 231.7136 127.7193 13.81411378 01
| Epoch (UTC): | 29 March 2026 05:17:14 |
| Eccentricity: | 0.0074622 |
| inclination: | 64.7003° |
| perigee height: | 904 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 61.7999° |
| argument of perigee: | 231.7136° |
| revolutions per day: | 13.81411378 |
| mean anomaly at epoch: | 127.7193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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