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 26041.92039929 +.00000000 +00000-0 +14905-3 0 00008
2 23705 71.0192 236.4559 0012087 170.2637 189.8722 14.15493939 02
| Epoch (UTC): | 10 February 2026 22:05:22 |
| Eccentricity: | 0.0012087 |
| inclination: | 71.0192° |
| perigee height: | 832 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 236.4559° |
| argument of perigee: | 170.2637° |
| revolutions per day: | 14.15493939 |
| mean anomaly at epoch: | 189.8722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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