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 62814U 26145.45267089 +.00000000 +00000-0 +56890-3 0 00004
2 62814 53.1598 312.8656 0001192 76.0761 284.0373 15.31721467 09
| Epoch (UTC): | 25 May 2026 10:51:50 |
| Eccentricity: | 0.0001192 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 312.8656° |
| argument of perigee: | 76.0761° |
| revolutions per day: | 15.31721467 |
| mean anomaly at epoch: | 284.0373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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