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 02825U 26073.61751834 +.00000000 +00000-0 +10207-3 0 00006
2 02825 69.9703 276.5726 0009639 287.7237 72.2817 13.97710275 00
| Epoch (UTC): | 14 March 2026 14:49:13 |
| Eccentricity: | 0.0009639 |
| inclination: | 69.9703° |
| perigee height: | 895 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 276.5726° |
| argument of perigee: | 287.7237° |
| revolutions per day: | 13.97710275 |
| mean anomaly at epoch: | 72.2817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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