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 62246U 26145.61501117 +.00000000 +00000-0 +11213-3 0 00004
2 62246 89.0105 24.7577 0016407 79.8160 280.4840 13.51005212 02
| Epoch (UTC): | 25 May 2026 14:45:36 |
| Eccentricity: | 0.0016407 |
| inclination: | 89.0105° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 24.7577° |
| argument of perigee: | 79.8160° |
| revolutions per day: | 13.51005212 |
| mean anomaly at epoch: | 280.4840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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