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 23659U 26088.10935752 +.00000000 +00000-0 +65476-4 0 00006
2 23659 82.5315 207.3526 0025018 172.4400 1.6047 14.80332998 05
| Epoch (UTC): | 29 March 2026 02:37:28 |
| Eccentricity: | 0.0025018 |
| inclination: | 82.5315° |
| perigee height: | 611 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 207.3526° |
| argument of perigee: | 172.4400° |
| revolutions per day: | 14.80332998 |
| mean anomaly at epoch: | 1.6047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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