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 62216U 26145.53508772 +.00000000 +00000-0 +76560-5 0 00004
2 62216 67.1469 105.9030 0006535 264.5508 95.4831 13.96671373 05
| Epoch (UTC): | 25 May 2026 12:50:31 |
| Eccentricity: | 0.0006535 |
| inclination: | 67.1469° |
| perigee height: | 901 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 105.9030° |
| argument of perigee: | 264.5508° |
| revolutions per day: | 13.96671373 |
| mean anomaly at epoch: | 95.4831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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