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 26022.30584977 +.00000000 +00000-0 +13653-3 0 00006
2 02825 69.9719 26.7265 0007603 337.6825 22.3950 13.97696074 01
| Epoch (UTC): | 22 January 2026 07:20:25 |
| Eccentricity: | 0.0007603 |
| inclination: | 69.9719° |
| perigee height: | 896 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 26.7265° |
| argument of perigee: | 337.6825° |
| revolutions per day: | 13.97696074 |
| mean anomaly at epoch: | 22.3950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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