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 02119U 26088.02649106 +.00000000 +00000-0 +18242-3 0 00008
2 02119 89.5993 91.8152 0144227 288.5192 70.0348 13.75386366 09
| Epoch (UTC): | 29 March 2026 00:38:08 |
| Eccentricity: | 0.0144227 |
| inclination: | 89.5993° |
| perigee height: | 874 km |
| apogee height: | 1086 km |
| right ascension of ascending node: | 91.8152° |
| argument of perigee: | 288.5192° |
| revolutions per day: | 13.75386366 |
| mean anomaly at epoch: | 70.0348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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