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 32395U 26142.17704933 +.00000000 +00000-0 +00000-0 0 00004
2 32395 64.3244 192.8648 0017122 356.1086 80.4224 2.13100136 04
| Epoch (UTC): | 22 May 2026 04:14:57 |
| Eccentricity: | 0.0017122 |
| inclination: | 64.3244° |
| perigee height: | 19086 km |
| apogee height: | 19174 km |
| right ascension of ascending node: | 192.8648° |
| argument of perigee: | 356.1086° |
| revolutions per day: | 2.13100136 |
| mean anomaly at epoch: | 80.4224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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