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 26022.13331988 +.00000000 +00000-0 -59876-4 0 00008
2 23705 71.0213 278.0002 0013284 201.0352 159.0226 14.15489351 09
| Epoch (UTC): | 22 January 2026 03:11:58 |
| Eccentricity: | 0.0013284 |
| inclination: | 71.0213° |
| perigee height: | 831 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 278.0002° |
| argument of perigee: | 201.0352° |
| revolutions per day: | 14.15489351 |
| mean anomaly at epoch: | 159.0226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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