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 00705U 26106.63439193 +.00000000 +00000-0 +82258-4 0 00007
2 00705 89.9207 70.8737 0035844 73.0573 105.7089 13.47666648 01
| Epoch (UTC): | 16 April 2026 15:13:31 |
| Eccentricity: | 0.0035844 |
| inclination: | 89.9207° |
| perigee height: | 1054 km |
| apogee height: | 1108 km |
| right ascension of ascending node: | 70.8737° |
| argument of perigee: | 73.0573° |
| revolutions per day: | 13.47666648 |
| mean anomaly at epoch: | 105.7089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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