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 32295U 26159.92427611 +.00000000 +00000-0 +38550-3 0 00003
2 32295 5.9384 176.4143 6696952 167.9912 223.9557 3.05162822 08
| Epoch (UTC): | 08 June 2026 22:10:57 |
| Eccentricity: | 0.6696952 |
| inclination: | 5.9384° |
| perigee height: | 254 km |
| apogee height: | 27146 km |
| right ascension of ascending node: | 176.4143° |
| argument of perigee: | 167.9912° |
| revolutions per day: | 3.05162822 |
| mean anomaly at epoch: | 223.9557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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