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 26038.03366161 +.00000000 +00000-0 +18300-3 0 00000
2 23705 71.0189 244.6166 0012370 176.1023 184.0199 14.15491427 07
| Epoch (UTC): | 07 February 2026 00:48:28 |
| Eccentricity: | 0.0012370 |
| inclination: | 71.0189° |
| perigee height: | 832 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 244.6166° |
| argument of perigee: | 176.1023° |
| revolutions per day: | 14.15491427 |
| mean anomaly at epoch: | 184.0199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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