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 23465U 26150.18831079 +.00000000 +00000-0 +33574-4 0 00000
2 23465 82.9289 36.5052 0036610 216.3932 258.3421 13.72024244 07
| Epoch (UTC): | 30 May 2026 04:31:10 |
| Eccentricity: | 0.0036610 |
| inclination: | 82.9289° |
| perigee height: | 965 km |
| apogee height: | 1019 km |
| right ascension of ascending node: | 36.5052° |
| argument of perigee: | 216.3932° |
| revolutions per day: | 13.72024244 |
| mean anomaly at epoch: | 258.3421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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