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 26044.90355450 +.00000000 +00000-0 +10677-3 0 00000
2 23704 70.9814 251.4267 0009880 332.8440 27.2164 14.13796704 07
| Epoch (UTC): | 13 February 2026 21:41:07 |
| Eccentricity: | 0.0009880 |
| inclination: | 70.9814° |
| perigee height: | 839 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 251.4267° |
| argument of perigee: | 332.8440° |
| revolutions per day: | 14.13796704 |
| mean anomaly at epoch: | 27.2164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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