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 00051U 26105.78347674 +.00000000 +00000-0 -21524-3 0 00007
2 00051 47.2123 242.4562 0107189 11.6964 348.6281 12.18377588 07
| Epoch (UTC): | 15 April 2026 18:48:12 |
| Eccentricity: | 0.0107189 |
| inclination: | 47.2123° |
| perigee height: | 1514 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 242.4562° |
| argument of perigee: | 11.6964° |
| revolutions per day: | 12.18377588 |
| mean anomaly at epoch: | 348.6281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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