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 62247U 26145.63969356 +.00000000 +00000-0 +13044-3 0 00004
2 62247 89.0101 24.8175 0016441 84.5887 275.7140 13.51006150 03
| Epoch (UTC): | 25 May 2026 15:21:09 |
| Eccentricity: | 0.0016441 |
| inclination: | 89.0101° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 24.8175° |
| argument of perigee: | 84.5887° |
| revolutions per day: | 13.51006150 |
| mean anomaly at epoch: | 275.7140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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