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 44874U 26088.07462734 +.00000000 +00000-0 +95047-4 0 00006
2 44874 98.1520 277.4543 0010404 357.9191 2.1965 14.61905599 02
| Epoch (UTC): | 29 March 2026 01:47:27 |
| Eccentricity: | 0.0010404 |
| inclination: | 98.1520° |
| perigee height: | 680 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 277.4543° |
| argument of perigee: | 357.9191° |
| revolutions per day: | 14.61905599 |
| mean anomaly at epoch: | 2.1965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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