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 62317U 26145.53440837 +.00000000 +00000-0 +39102-3 0 00002
2 62317 53.1577 183.8827 0001106 92.1878 267.9249 15.30209785 08
| Epoch (UTC): | 25 May 2026 12:49:32 |
| Eccentricity: | 0.0001106 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 183.8827° |
| argument of perigee: | 92.1878° |
| revolutions per day: | 15.30209785 |
| mean anomaly at epoch: | 267.9249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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