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 62156U 26145.53178515 +.00000000 +00000-0 +53430-3 0 00004
2 62156 43.0022 83.9984 0000998 279.9266 80.1473 15.27584839 06
| Epoch (UTC): | 25 May 2026 12:45:46 |
| Eccentricity: | 0.0000998 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 83.9984° |
| argument of perigee: | 279.9266° |
| revolutions per day: | 15.27584839 |
| mean anomaly at epoch: | 80.1473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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