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 10974U 26105.73867127 +.00000000 +00000-0 +25017-4 0 00008
2 10974 82.4834 351.8120 0018028 86.5465 273.7815 14.90051288 06
| Epoch (UTC): | 15 April 2026 17:43:41 |
| Eccentricity: | 0.0018028 |
| inclination: | 82.4834° |
| perigee height: | 585 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 351.8120° |
| argument of perigee: | 86.5465° |
| revolutions per day: | 14.90051288 |
| mean anomaly at epoch: | 273.7815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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