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 62956U 26145.51486057 +.00000000 +00000-0 +27106-3 0 00004
2 62956 53.1601 233.2165 0001189 79.3088 280.8048 15.33549717 07
| Epoch (UTC): | 25 May 2026 12:21:23 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.1601° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 233.2165° |
| argument of perigee: | 79.3088° |
| revolutions per day: | 15.33549717 |
| mean anomaly at epoch: | 280.8048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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