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 26104.06101647 +.00000000 +00000-0 -60072-3 0 00006
2 00051 47.2124 247.7862 0107258 6.6093 353.6084 12.18377692 06
| Epoch (UTC): | 14 April 2026 01:27:51 |
| Eccentricity: | 0.0107258 |
| inclination: | 47.2124° |
| perigee height: | 1514 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 247.7862° |
| argument of perigee: | 6.6093° |
| revolutions per day: | 12.18377692 |
| mean anomaly at epoch: | 353.6084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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