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 23522U 26149.59494544 +.00000000 +00000-0 +00000-0 0 00003
2 23522 14.2908 4.5733 0005927 152.8531 38.4577 0.99401874 06
| Epoch (UTC): | 29 May 2026 14:16:43 |
| Eccentricity: | 0.0005927 |
| inclination: | 14.2908° |
| perigee height: | 36007 km |
| apogee height: | 36057 km |
| right ascension of ascending node: | 4.5733° |
| argument of perigee: | 152.8531° |
| revolutions per day: | 0.99401874 |
| mean anomaly at epoch: | 38.4577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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