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 23705U 26037.96299355 +.00000000 +00000-0 +18358-3 0 00004
2 23705 71.0189 244.7649 0012378 176.1899 183.9321 14.15491393 00
| Epoch (UTC): | 06 February 2026 23:06:42 |
| Eccentricity: | 0.0012378 |
| inclination: | 71.0189° |
| perigee height: | 832 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 244.7649° |
| argument of perigee: | 176.1899° |
| revolutions per day: | 14.15491393 |
| mean anomaly at epoch: | 183.9321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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