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 23704U 26162.56362105 +.00000000 +00000-0 -96080-4 0 00002
2 23704 70.9865 4.6376 0009134 181.8530 178.2559 14.13823817 07
| Epoch (UTC): | 11 June 2026 13:31:36 |
| Eccentricity: | 0.0009134 |
| inclination: | 70.9865° |
| perigee height: | 840 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 4.6376° |
| argument of perigee: | 181.8530° |
| revolutions per day: | 14.13823817 |
| mean anomaly at epoch: | 178.2559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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