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 23464U 26148.42604670 +.00000000 +00000-0 +10692-3 0 00003
2 23464 82.9293 33.2596 0040188 202.0895 157.8530 13.73079274 01
| Epoch (UTC): | 28 May 2026 10:13:30 |
| Eccentricity: | 0.0040188 |
| inclination: | 82.9293° |
| perigee height: | 959 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 33.2596° |
| argument of perigee: | 202.0895° |
| revolutions per day: | 13.73079274 |
| mean anomaly at epoch: | 157.8530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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