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 26073.05686197 +.00000000 +00000-0 +44462-3 0 00002
2 00051 47.2161 343.7236 0108934 274.7760 84.0597 12.18377151 04
| Epoch (UTC): | 14 March 2026 01:21:52 |
| Eccentricity: | 0.0108934 |
| inclination: | 47.2161° |
| perigee height: | 1513 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 343.7236° |
| argument of perigee: | 274.7760° |
| revolutions per day: | 12.18377151 |
| mean anomaly at epoch: | 84.0597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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