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 28522U 26021.37618144 +.00000000 +00000-0 +10036-3 0 00000
2 28522 82.9481 133.3544 0044043 291.5589 68.0885 13.90041554 07
| Epoch (UTC): | 21 January 2026 09:01:42 |
| Eccentricity: | 0.0044043 |
| inclination: | 82.9481° |
| perigee height: | 896 km |
| apogee height: | 961 km |
| right ascension of ascending node: | 133.3544° |
| argument of perigee: | 291.5589° |
| revolutions per day: | 13.90041554 |
| mean anomaly at epoch: | 68.0885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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