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 25119U 26088.01129661 +.00000000 +00000-0 +46183-3 0 00006
2 25119 45.0132 79.3571 0004002 250.4758 109.5662 14.47338080 01
| Epoch (UTC): | 29 March 2026 00:16:16 |
| Eccentricity: | 0.0004002 |
| inclination: | 45.0132° |
| perigee height: | 732 km |
| apogee height: | 737 km |
| right ascension of ascending node: | 79.3571° |
| argument of perigee: | 250.4758° |
| revolutions per day: | 14.47338080 |
| mean anomaly at epoch: | 109.5662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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