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 26019.16525882 +.00000000 +00000-0 -61237-4 0 00009
2 23705 71.0221 284.2313 0013451 205.5562 154.4898 14.15489644 09
| Epoch (UTC): | 19 January 2026 03:57:58 |
| Eccentricity: | 0.0013451 |
| inclination: | 71.0221° |
| perigee height: | 831 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 284.2313° |
| argument of perigee: | 205.5562° |
| revolutions per day: | 14.15489644 |
| mean anomaly at epoch: | 154.4898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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