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 26064.74612336 +.00000000 +00000-0 +85534-4 0 00009
2 23705 71.0213 188.5336 0010969 132.7336 227.4712 14.15493138 01
| Epoch (UTC): | 05 March 2026 17:54:25 |
| Eccentricity: | 0.0010969 |
| inclination: | 71.0213° |
| perigee height: | 833 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 188.5336° |
| argument of perigee: | 132.7336° |
| revolutions per day: | 14.15493138 |
| mean anomaly at epoch: | 227.4712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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