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 14051U 26068.45746736 +.00000000 +00000-0 +47415-3 0 00002
2 14051 25.3274 93.9808 0985169 175.5262 185.4819 13.34346260 07
| Epoch (UTC): | 09 March 2026 10:58:45 |
| Eccentricity: | 0.0985169 |
| inclination: | 25.3274° |
| perigee height: | 391 km |
| apogee height: | 1870 km |
| right ascension of ascending node: | 93.9808° |
| argument of perigee: | 175.5262° |
| revolutions per day: | 13.34346260 |
| mean anomaly at epoch: | 185.4819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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