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 62327U 26145.61332691 +.00000000 +00000-0 +76436-4 0 00002
2 62327 86.5045 351.0622 0001361 90.6959 269.4331 13.24408557 05
| Epoch (UTC): | 25 May 2026 14:43:11 |
| Eccentricity: | 0.0001361 |
| inclination: | 86.5045° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 351.0622° |
| argument of perigee: | 90.6959° |
| revolutions per day: | 13.24408557 |
| mean anomaly at epoch: | 269.4331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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