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 23711U 26073.56711995 +.00000000 +00000-0 +97626-4 0 00002
2 23711 100.5066 103.5378 0367080 310.3249 167.1164 13.12852155 06
| Epoch (UTC): | 14 March 2026 13:36:39 |
| Eccentricity: | 0.0367080 |
| inclination: | 100.5066° |
| perigee height: | 934 km |
| apogee height: | 1491 km |
| right ascension of ascending node: | 103.5378° |
| argument of perigee: | 310.3249° |
| revolutions per day: | 13.12852155 |
| mean anomaly at epoch: | 167.1164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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