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 14452U 26088.23478994 +.00000000 +00000-0 +71383-4 0 00005
2 14452 81.1582 77.8348 0091051 75.0319 286.0918 14.27254594 08
| Epoch (UTC): | 29 March 2026 05:38:05 |
| Eccentricity: | 0.0091051 |
| inclination: | 81.1582° |
| perigee height: | 736 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 77.8348° |
| argument of perigee: | 75.0319° |
| revolutions per day: | 14.27254594 |
| mean anomaly at epoch: | 286.0918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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