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 26100.16492894 +.00000000 +00000-0 +50319-4 0 00008
2 10974 82.4842 357.1136 0017976 103.4737 256.8487 14.90048413 06
| Epoch (UTC): | 10 April 2026 03:57:29 |
| Eccentricity: | 0.0017976 |
| inclination: | 82.4842° |
| perigee height: | 585 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 357.1136° |
| argument of perigee: | 103.4737° |
| revolutions per day: | 14.90048413 |
| mean anomaly at epoch: | 256.8487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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