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 23704U 26018.51286375 +.00000000 +00000-0 -95069-4 0 00007
2 23704 70.9873 306.7819 0008900 6.5967 353.5271 14.13800007 06
| Epoch (UTC): | 18 January 2026 12:18:31 |
| Eccentricity: | 0.0008900 |
| inclination: | 70.9873° |
| perigee height: | 840 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 306.7819° |
| argument of perigee: | 6.5967° |
| revolutions per day: | 14.13800007 |
| mean anomaly at epoch: | 353.5271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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