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 17070U 26106.70655105 +.00000000 +00000-0 +82000-4 0 00006
2 17070 89.6242 178.8254 0041504 103.2304 68.4011 13.75278238 06
| Epoch (UTC): | 16 April 2026 16:57:26 |
| Eccentricity: | 0.0041504 |
| inclination: | 89.6242° |
| perigee height: | 950 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 178.8254° |
| argument of perigee: | 103.2304° |
| revolutions per day: | 13.75278238 |
| mean anomaly at epoch: | 68.4011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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